N836RA

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 42,807 hrs · 35,155 cycles

AFT CARGO FIRE LOOP B LIGHT ILLUMINATED INFLIGHT & WOULD NOT GO OUT AFTER QRH PROCEDURES.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 42,692 hrs · 35,079 cycles

AFTER DEPARTING KLCK WITH NORMAL PROCEDURES, WE NOTICED THE FLOW LIGHT ILLUMINATED. STOP CLIMB AT 230 & RAN QRH, UNABLE TO MAINTAIN CABIN PRESS & RETURNED TO KLCK.

Part: SWITCH — BROKEN (PA PHONE) · airframe 42,692 hrs · 35,079 cycles

COCKPIT PA PHONE PTT SWITCH ON HANDSET BROKEN & INOPERATIVE.

Part: SPEAKER — BROKEN (CABIN) · airframe 42,674 hrs · 35,067 cycles

L2 JUMP SEAT SPEAKER BROKEN.

Part: ENGINE — FAILED (RIGHT)

AFTER TAKEOFF, RT ENGINE EGT STABILIZED AT 600 DEGREES FOR 10 SECONDS AFTER V1 AND ATC REPORTED SPARKS COMING FROM THE LT ENGINE. A PRECAUTIONARY LANDING WAS EXECUTED WITH NO FURTHER EVENT.

Part: HEADSET — FAILED (COCKPIT) · airframe 42,593 hrs · 34,999 cycles

F/O HEADSET WONT TRANSMIT. REPLACED F/O HEADSET, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 42,532 hrs · 34,957 cycles

WHEN OPENING L2 DOOR TO CLEAN TRASH FROM GALLEY THE DOOR SLIDE WAS DEPLOYED. R & R L2 DOOR SLIDE IAW MM 25-62-00.

Part: LATCH — OUT OF ADJUST (CARGO DOOR) · airframe 42,458 hrs · 43,910 cycles

AT 800AGL MID CARGO DOOR LIGHT CAME ON. ADJUSTED MID CARGO DOOR LATCH IAW AMM AND LIGHT EXTINGUSHED.

Part: PA SYSTEM — WEAK (CABIN) · airframe 42,421 hrs · 34,887 cycles

FLIGHT DECK PA VERY LOW CAN NOT BE HEARD AND STATIC SOUNDS.

Part: INTERPHONE — INOPERATIVE · airframe 42,337 hrs · 34,854 cycles

FLIGHT DECK TO CABIN INTERPHONE DIFFICULT TO HEAR.

Part: PA SYSTEM — INOPERATIVE · airframe 42,315 hrs · 34,845 cycles

AFT PA-RC DID NOT OPERATE IN FLIGHT OR ON GROUND.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 42,315 hrs · 34,845 cycles

NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF. NOSE GEAR PINNED.

Part: PA SYSTEM — NONE · airframe 42,302 hrs · 34,840 cycles

FLIGHT DECK TO CABIN PA INAUDIBLE (TO LOW). C/W WITH OPS CHECK OF PA SYS, FOUND NO FAULTS AT THIS TIME IAW AMM 23-30-01.

Part: PA SYSTEM — INOPERATIVE · airframe 41,654 hrs · 21,500 cycles

L1 DOOR P/A VOLUME IS LOW.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 42,265 hrs · 34,823 cycles

CAPTAINS AIRSPEED INDICATOR WAS INOPERATIVE DURING TAKEOFF, ABORTED TAKEOFF.

Part: INTERPHONE — INOPERATIVE (COCKPIT) · airframe 42,203 hrs · 34,793 cycles

COCKPIT INTERPHONE NOT TRANSMITTING.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 42,178 hrs · 34,780 cycles

NR 2 ENGINE START VALVE OPEN LIGHT ON, NO ENGINE ROTATION.

Part: UNKNOWN — UNKNOWN (INTERPHONE) · airframe 42,159 hrs · 34,772 cycles

R/C INTERPHONE VOLUME TOO LOW, CAN NOT HEAR WHEN CALLING FROM THE FRONT (L1 DOOR).

Part: UNKNOWN — FAULTY (PA SYSTEM) · airframe 42,159 hrs · 34,772 cycles

CAN NOT HEAR PA IN FLIGHT WHEN FLIGHT DECK CALLS CABIN, PA WORKS ON GROUND.

Part: PA SYSTEM — MALFUNCTIONED · airframe 42,003 hrs · 34,685 cycles

P/A INOPERATIVE IN FLIGHT. OPS CHECKED NORMAL ON GROUND COULD NOT DUPLICATE FAULT ON GROUND.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

G5 GALLEY BOTTOM SUPPORT STRUCTURE U CHANNELS CORRODED. R & R 3 EA U CHANNELS IAW SRM 51-30-2.

Part: WEB — CRACKED (ZONE 200) · airframe 41,977 hrs · 34,570 cycles

CRACKED CANTED WEB AT BS 1485 UPPER RT SIDE. REMOVED CRACKED WEB IAW SRM 51-30-05. FABRICATED WEB IAW SRM 51-10-3. INSTALLED WEB IAW SRM 51-30-01.

Part: CHANNEL — CORRODED (ZONE 200) · airframe 41,977 hrs · 34,507 cycles

G4 GALLEY NUMEROUS U CHANNELS CORRODED. R & R NUMEROUS U CHANNELS IAW SRM 51-30-2

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

G4 GALLEY BOTTOM STRUCTURE U CHANNEL BENT AND CORRODED. R & R U CHANNEL IAW SRM 51-30-1.

Part: BRACKET — CRACKED (ZONE 100) · airframe 41,977 hrs · 34,570 cycles

RT LOWER ATTACHED BRACKET OF HANDRAIL CRACKED. FABRICATED NEW BRACKET FROM 2024 T3 IAW SRM 51-10-2. INSTALLED NEW BRACKET IAW SRM 51-30-2.

Part: TORQUE TUBE — WORN (RUDDER TAB) · airframe 41,977 hrs · 34,570 cycles

RUDDER CONTROL TAB TORQUE TUBE HAS EXCESSIVE PLAY WHERE IT EXITS THE RUDDER DRIVE TORQUE TUBE, ACFT SIDE. REMOVED RUDDER DRIVE TORQUE TUBE AND RUDDER CONTOL TAB TORQUE TUBE. AFTER EVALUATION MANY COMPONENTS FOUND TO WORN BEYOUND SERVICEABLE LIMITS. REPLACED RUDDER TORQUE TUBE AND BEARING IAW MM 27-20-03. REPLACED RUDDER SECTOR PIVOT ATTACHED BEARING IAW SOPM 20-50-03. REPLACED RUDDER HYD POWER PACKAGE DRIVE SECTOR PUSHRODS IAW SOPM 20-50-03. REINSTALLED ALL REMOVED COMPONENTS AND FUNCTIONAL TESTED ALL SYSTEM IAW MM 27-20-02, SYS OPS CHECKS NORMAL.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

LT LAV AREA BETWEEN FLOORBEAM AT BS 1309 CARGO CEILING PANEL ATTACH STRAP CORRODED. REMOVED CORRODED STRAP, FABRICATED AND INSTALLED REPAIR STRAP IAW SRM 51-30-0.

Part: SKIN — CRACKED (ZONE 100) · airframe 41,977 hrs · 34,570 cycles

CRACK INDICATION AT BS 69.5 LONGERON 20 TO 21 LT SIDE SKIN. REMOVED ELEVEN RIVETS AT BS 69.5 AT LONGERON 20 TO 21 LT SIDE IAW SRM 51-10-4. REMOVED DAMAGE SKIN IAW SRM 53-04-02. FABRICATED LOCATED AND DRILLED REPAIR DOUBLER IAW SRM 51-10-04. INSTALLED REPAIR DOUBLER IAW SRM 53-04-02.

Part: CHANNEL — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

AFT ENTRY DOOR HAT CHANNEL CORRODED. REMOVED CORRODED HAT CHANNEL IAW SRM 51-10-3A. FABRICATED REPAIR ANGLE IAW 51-10-2. DRILLED AND LOCATED REPAIR ANGLE IAW SRM 51-70-5. INSTALLED REPAIR ANGLE IAW SRM 51-30-8.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 41,978 hrs · 34,671 cycles

UNABLE TO MAINTAIN CABIN PRESSURE ON SINGLE PACK, REFER TO L.P. 65738. DIFF .5 AT 12,000 FEET, FLOW LIGHT CABIN ON AT 14,000. DURING CLIMB - INTERMITTENT, STEADY AT FL 210, CABIN CONTINUED CLIMBING, AT CABIN ALTTITUDE 10,000 INTO DESC RT PACK FLOW 3.5 PSI.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

FWD CARGO COMPARTMENT RT SIDE FLOOR SUPPORT, FASTENER HOLES ARE CORRODED AND ALL HOLES ARE BLOWN OUT. REMOVED FLOOR SUPPORT IAW SRM 51-30-1. RECEIVED AND FABRICATED PART AND ALODINE AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR SUPPORT IAW SRM 51-30-01.

Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

AFT CARGO BAY RETAINING STRIPS HAVE SURFACE CORROSION. REMOVED CORRODED RETAINING STRIPS AND FABRICATED REPLACEMENT STRIPS AND INSTALLED REPLACEMENT STRIPS IAW SRM 51-10-04.

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 41,977 hrs · 34,570 cycles

LT UPPER HORIZONTAL STABILIZER FAIRING, UPPER ATTACH ANGLES CRACKED AT FASTENERS HOLES. FABRICATED REPAIR ANGLES IAW SRM 51-10-2. LOCATED AND DRILLED THE FORWARD AND AFT ANGLE IAW SRM 51-10-04. INSTALLED NEW ANGLES IAW SRM 51-30-2.

Part: ATTACH ANGLE — BROKEN (ZONE 300) · airframe 41,977 hrs · 34,570 cycles

LEFT HORIZONTAL STAB AFT ATTACH CHANNEL BROKEN AT STAB, APPROX STA 56. REMOVED BROKEN ATTACHED CHANNEL ON LT HORZ STAB IAW SRM 51-30-2. FABRICATED REPLACEMENT ATTACH ANGLES, LOCATED, DRILLED AND INSTALLED IAW SRM 51-30-8, 51-10-04 AND 51-10-2.

Part: STRIP — CRACKED (ZONE 100) · airframe 41,977 hrs · 34,570 cycles

FWD CARGO LT SIDE TUNNEL PANEL SUPPORT CENTER STRIP CRACKED AT STA 218 THROUGH 219. FABRICATED REPLACEMENT SUPPORT STRIP IAW SRM 51-10-2. INSTALLED REPLACEMENT SUPPORT STRIP IAW SRM 51-30-2.

Part: ATTACH ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

LEFT LAV FLOOR TO WALL ATTACH ANGLES HAVE SURFACE CORROSION. R & R 3 EA ATTACH ANGLES IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,977 hrs · 34,570 cycles

CORROSION ON FLOORBOARD SUPPORT ANGLE ATTACHED TO AFT CARGO MAIN FRAME BILGE AREA STA 1079 AND RBL 13. REMOVED FLOOR SUPPORT IAW SRM 51-30-05, CORROSION IS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-05.

Part: SENSOR — MALFUNCTIONED (OVERHEAT LOOP) · airframe 41,950 hrs · 34,651 cycles

TAIL CONE OVERHEAT LIGHT ON AT 220 WOULD NOT EXTINQUISH, "FLICKERING". R & R LT & RT OVERHEAT SENSORS IAW MM 36-20-02. OPS CKD GOOD.

Part: SENSOR — INOPERATIVE (OVERHEAT LOOP) · airframe 41,950 hrs · 34,651 cycles

TAIL CONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH FLICKERING. R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.

Part: SENSOR — INTERMITTENT (OVERHEAT LOOP) · airframe 41,950 hrs · 34,651 cycles

TAILCONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH FLICKERING. R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02, OPS CKD GOOD.

Part: SENSOR — INOPERATIVE (OVERHEAT SYS) · airframe 41,950 hrs · 34,651 cycles

TAILCONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH "FLICKERING". R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.

Part: SENSOR — FAILED (TAILCONE) · airframe 41,950 hrs · 34,651 cycles

TAIL CONE OVERHEAT LIGHT ON AT 220 DEGREES WOULD NOT EXTINGUISH. R & R LT AND RT OVERHEAT SENSORS IAW AMM 36-20-02. OPS CHECKED GOOD.

Part: SENSOR — INTERMITTENT (OVERHEAT LOOP) · airframe 41,950 hrs · 34,651 cycles

TAIL CONE OVERHEAT LIGHT ON AT 220, WOULD NOT EXTINQUISH, FLICKERING". R & R LT & RT OVERHEAT SENSOR IAW MM 36-20-02. OPS CKD GOOD.

Part: WARNING LIGHT — ILLUMINATED (CSD) · airframe 40,141 hrs · 41,098 cycles

AT FL310 THE RIGHT LOW CSD LIGHT CAME ON. PERFORMED THE QRH EMERGENCY CHECKLIST.

Part: SKIN — DAMAGED (THRUST REVERSER) · airframe 41,629 hrs · 34,428 cycles

SKIN DAMAGED RT THRUST REVERSER ACCUMULATOR SERVICE DOOR, INSTALLED TEMPORY REPAIR IAW SRM 53-04-02.

Part: LANDING GEAR — FAILED · airframe 41,592 hrs · 34,413 cycles

LANDING GEAR WOULD RETRACT AFTER TAKEOFF, RETURN TO AIRPORT.

Part: LANDING GEAR — INOPERATIVE · airframe 41,592 hrs · 34,413 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, RETURNED TO ORIGINATING AIRPORT.

Part: WARNING LIGHT — ILLUMINATED (OIL FILTER) · airframe 41,525 hrs · 34,387 cycles

OIL FILTER CLOG LIGHT, RT ENG CAME ON BRIEFLY WENT OUT BEFORE ANY ACTION TAKEN.

Part: WARNING LIGHT — INTERMITTENT · airframe 41,525 hrs · 34,387 cycles

"OIL CLOG LT" RT ENG CAME ON BRIEFLY, WENT OUT BEFORE ANY ACTION TAKEN.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 41,526 hrs · 34,388 cycles

PA SYSTEM INOPERATIVE AT L1 TO R1 AND L2 DOORS.

Part: AMPLIFIER — OUT OF ADJUST (INTERPHONE) · airframe 41,526 hrs · 34,388 cycles

P/A INTERPHONE VOLUME LOW: ADJUSTED VOLUME ON PA AMPLIFIER, OPS GOOD.

Part: HANDSET — INOPERATIVE (PA SYSTEM) · airframe 41,525 hrs · 34,387 cycles

FWD F/A HANDSET INOPERATIVE, PA.

Part: HANDSET — INOPERATIVE (PA SYSTEM) · airframe 41,525 hrs · 34,387 cycles

FWD F/A PA HANDSET INOPERATIVE.

Part: HANDSET — WEAK · airframe 41,473 hrs · 34,367 cycles

F/A HANDSET AT L-2 DOOR STATION IS WEAK.

Part: HANDSET — WEAK (CABIN) · airframe 41,473 hrs · 34,367 cycles

F/A HANDSET AT L2 DOOR STATION IS WEAK.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 41,315 hrs · 34,306 cycles

INTERPHONE DOES NOT WORK AT L2.

Part: INTERPHONE — INOPERATIVE (L2 DOOR) · airframe 41,315 hrs · 34,306 cycles

INTERPHONE DOES NOT WORK L2.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,229 hrs · 34,260 cycles

CORROSION ON THE FLOOR SUPPORT STURCTURE AT BODY STATION 140 TO 155. REMOVED CORROSION FROM FLOOR SUPPORT IAW MD-80 SROM 51-10-3 PAGE 26. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-10-4, PAGE 2. INSTALLED REPAIR PARTS IAW SRM 51-30-1.

Part: MOUNT BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 41,229 hrs · 34,260 cycles

R1 DOOR, FORWARD AND AFT GIRT BAR MOUNTING BRACKETS ARE CORRODED. REMOVED CORROSION FROM THE R1 DOOR FORWARD AND AFT GIRT BAR MOUNTING BRACKET. AFTER EVALUATION IT WAS DETERMIND THE CORROSION ON THE BRACKETS WAS OUT OF LIMITS. REPLACED THE FORWARD AND AFT GIRT BAR FITTINGS IAW SRM 51-10-4.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,229 hrs · 34,260 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE AT BODY STATION 208 AT LBL6 LT. REMOVED CORROSION FROM THE LT INBD FLOOR SUPPORT AT BODY STATION 208 LBL 6 IAW SRM 51-10-3 PARA 26. SUPPORT FOUND TO BE OUT OF LIMITS. RECEIVED REPLACEMENT EXTRUSION, LOCATED AND DRILLED IAW SRM 51-10-04. INSTALLED REPAIR EXTRUSION AT FLOOR SUPPORT IAW SRM 51-30-1, PAGE 13.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 41,139 hrs · 34,204 cycles

L-2 INTERPHONE INOPERATIVE DURING FLIGHT.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 41,139 hrs · 34,204 cycles

L2 INTERPHONE INOPERATIVE DURING FLIGHT.

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 41,097 hrs · 34,168 cycles

NOSE GEAR UNSAFE LIGHT INDICATION WAS ON AFTER TAKEOFF. CYCLED THREE TIMES AND WAS STILL ON.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 41,097 hrs · 34,168 cycles

NOSE UNSAFE LIGHT INDICATION WAS ON AFTER TAKEOFF. RECYCLED THREE TIMES AND WAS STILL ON.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 41,089 hrs · 34,165 cycles

INOPERATIVE EMERGENCY LIGHT AFT NON STANDARD DROP CEILING PANEL & AFT STANDARD DROP PANEL. FOUND BATTERY BS-27 TO HAVE OV. R & R BATTERY IAW MM 33-53-00 PG 407-411. OPS CHECKED GOOD IAW MM 33-53-00, PGS 501-503.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,089 hrs · 34,165 cycles

INOPERATIVE DROP CEILING LIGHT, AFT NON STANDARD DROP CEILING PANEL AND AFT DROP CEILING PANEL: FOUND BATTERY BS-27 OVER VOLTAGE, R & R BATTERIES IAW AMM 33-53-00, PG 407-411, OPS CHECKED GOOD IAW AMM 33-53-00, PG 501-503.

Part: WARNING LIGHT — ILLUMINATED (OIL FILTER) · airframe 41,036 hrs · 34,121 cycles

ON ARRIVAL, CAPTAIN REPORTED AN INFLIGHT OIL FILTER CLOGGED LIGHT ILLUMINATED, ACCOMPLISHED QRH PROCEDURES AND LIGHT WOULD NOT EXTINGUISH, FOLLOWED QRH PROCEDURES AND SHUTDOWN NR 2 ENGINE. ACFT LANDED WITHOUT INCIDENT, NO EMERGENCY LANDING WAS DECLAIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,036 hrs · 40,901 cycles

FWD ENTRY AND L1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERY PACK IAW MM 33-53-00. OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,036 hrs · 40,901 cycles

EMERGENCY LIGHT BATTERY PACK AT BS 219 INOPERATIVE. R & R EMERGENCY BATTERY PACK. OPS CHECKED NORMAL IAW AMM 33-53-00.

Part: JACK — LOOSE (INTERPHONE) · airframe 40,935 hrs · 34,043 cycles

COCKPIT INTERCOM BETWEEN CAPT AND F/O INOP. FOUND INTERCOM WEAK DUE TO LOOSE PLUG AT F/O'S JACK PANEL. RESECURED, OPS CHECK GOOD IAW MM 23-50-05.

Part: CONNECTOR — UNSECURE (INTERCOM) · airframe 40,935 hrs · 34,043 cycles

COCKPIT INTERCOM BETWEEN CAPT AND F/O INOPERATIVE. FOUND INTERCOM WEAK DUE TO LOOSE CONNECTOR AT F/O'S JACK PANEL. SECURED, OPS CHECKED GOOD IAW AMM 23-0-05.

Part: SEAL — LOOSE (L2 DOOR) · airframe 39,735 hrs · 33,308 cycles

AFTER TAKEOFF ACFT FAILED TO PRESSURIZE. A/C RETURNED BACK TO DEPARTURE. UPON PARKING MX DISCOVERED THE L-2 DOOR SEAL HAD COME OFF OF IT'S RETAINER.

Part: INSTRUMENT PANEL — MULTIPLE FAIL · airframe 39,681 hrs · 32,267 cycles

DURING CRUISE FLT, CREW REPORTED, LOST BOTH NR1 AND NR2 DFGC. NO AUTO PILOT, NO AUTO THROTTLES, NO FLIGHT DIRECTORS. DISPATCH WAS ADVISED, ADVISED AND REROUTED ACFT FOR REPAIRS.

Part: ENGINE — OVERTEMP (LEFT) · airframe 38,701 hrs · 32,645 cycles

ON TAKEOFF, LT ENGINE DID NOT REACH TO POWER, EGT REACHED 630 DEGRESS AT APPROX 94 PERCENT N1. REQUIRED N1 AT 1,000 FT AND 26 DEGRESS IS 97.1 PERCENT. BOTH PILOT'S SAW EXCESSIVE EGT AND ABORTED TAKEOFF AT APPROX 30-40 KTS.

Part: BOTTLE — EMPTY (OXYGEN SYSTEM) · airframe 38,456 hrs · 32,519 cycles

ON TERMINATION OF FLIGHT, DURING PARKING CHECK LIST FOUIND OXYGEN CYLINDER PRESSURE AT 0 PSI.

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS AT STA 213 CEILING ARE DIM.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 37,583 hrs · 32,085 cycles

FLAPS TAKE OFF WARNING UPON BEGINNING OF TAKE OFF ROLL. RETURN TO THE GATE.

Part: HANDSET — INOPERATIVE (PA SYSTEM) · airframe 37,532 hrs · 32,061 cycles

COCKPIT PA HANDSET DOES NOT BROADCAST TO CABIN.

Part: SWITCHING UNIT — DEFECTIVE (PA SYSTEM) · airframe 37,463 hrs · 32,020 cycles

COCKPIT PA IS INTERMITTENT. SWITCHING UNIT REPLACED.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 36,850 hrs · 31,488 cycles

THROUGH FLIGHT LEVEL 240 LET ENGINE EPR WAS 1.60 AND RT ENG WAS 2.70 WE SHUTDOWN THE LT ENG AND AFTER SHUTDOWN THE LT ENG AND AFTER SHUTDOWN THE PARAMETERS WERE OK FOR THAT CONDITION AFTER AIRSTART THE PARAMETERS IN IDLE WERE NORMAL AFTER ACCELERATE THE L ENGINE AND PASSING THROUGH 1.60 EPR ALL THE PARAMETERS N1,EGT,N2,FF FREEZE NORMAL AND THE ENG DIDN’T ACCELERATE EVEN IF THE LT THROTTLE WAS ON FIREWALL OR IDLE. IAW AMM 73-12-01 PAGE 201 CONF 3 FUEL PUMP IAW AM 73-02-01 CONF 1 PAGE 201 FCU WAS REPLACED IAW AMM 72-00-00 CONF 8 PAG 501. RUN UP WAS DONE

Part: AHRS — FAILED (NR 1) · airframe 32,996 hrs · 27,785 cycles

AFTER T/O TO 30º AHRS DIFERENCE WAS PRESENTED. AFTER THAT TOTAL AHRS FAILURE CHECK LIST WAS PERFORMED UNSATISFACTORY IAW AMM 34-20-00 PAGE 401 WAS SWAPPED THE AHRS NR 1 WITH ANRS NR 2 AND PERFORMED BITE PROCEDURE AMM 34-22 03 PAGE 201. TEST ON GROUND SATISFACTORY, P/N ON 460800-03-06 S/N POS 1 ON 1548 ON S/N POS 2 ON 1135 ON P/N ON - OFF:460800-03-06 S/N OFF: POS (1)1135 S/N OFF: POS (2) 1548.

Part: VALVE — FAILED · airframe 32,022 hrs · 26,849 cycles

AFTER FIRST TURN, HEADING COMPARATOR FLAG CAME ON AND THERE WAS A DIFFERENCE BETWEEN AHRS OF 17 GRADE AND NO HEADING DISPLAY ON FMA AND NO AUTO PILOT WERE AVAILABLE. IAW AMM 34-21-06/201 IT WAS REMOVED AND REPLACED FLUX VALVE NR 1 COMPASS SWING IS ALIGNED, TEST SATISFACTORY.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 31,660 hrs · 26,530 cycles

PILOT REPORT: ONE MINUTE AFTER TAKEOFF, LT ENGINE COMPRESSOR STALL WAS PRESENTED AND A STRONG SHAKE ON THE AIRPLANE WAS FELT. LT THROTTLE LEVER WAS REDUCED UNTIL COMPRESSOR STALL STOPPED. ENGINE COMPRESSOR STALL CHECK LIST WAS PERFORMED A NORMAL LANDING WAS PERFORMED. CORRECTIVE ACTIONS: THE C1.5--C7TH--C6TH COMPRESSOR BLADES STAGE, BORESCOPE INSPECTION WAS PERFORMED NO DISCREPANCIES WERE FOUND. THE C1 WAS CHECKED WITH 2 BLADES OUT OF LIMITS IAW AMM-72-33-02/P 401 THE C1 WAS REPLACED P4151631-X1: THE INLET CASE MUST BE CHANGED IN LT ENGINE, IAW AMM 72-23-02 P/401 THE INLET CASE WAS REPLACED. IN LT ENGINE; P4151631-X2 : THE NOSE COWL REQUIRED CHANGE IN LT ENGINE : IAW AMM 71-10-01 P/201 THE NOSE COWL WAS REPLAC

Part: UNKNOWN — MULTIPLE FAIL · airframe 31,234 hrs · 26,136 cycles

AT FL 330, WITH AIRFOIL AND ENG ANTI-ICE ON, R ICE PROT TEMP LOW ANNUNCIATION CAME ON WITH 22 PSI WITH RT CABIN TEMP IN AUTO MODE AFTER 10 MIN R PACK WAS TRIPPED AND PRESS DROPPED TO 0, ABNORM PROCEDURE PERFORMED, WITH UNSATISFACTORY RESULT WITH R PACK TRIPPED, FLOW LIGHT CAME ON. PROCEDURES WERE MADE WITH UNSATISFACTORY RESULT. A/C STARTED TO DECOMPRESS AND EMERG PROCEDURES WERE CONDUCTED. CABIN ALT STABILIZED AT 12000 FT. IAW AMM 21-00-00 PG 501 BLEED A/C TEST WAS PERFORMED IAW AMM 21-32-00 PG 201 TO 209 CABIN PRESS CONTROLLERS CHECKED FOR FAULT IND AND PRESS CONTROL. NO SHOW FAULT WITH APU PRESS IN RT DUCTS AND PACK WAS FOUND LEAKS. ONE CLAMP WAS REPLACED AND OTHERS TIGHTENED. TEST ON GROUND SATIS.

Part: START VALVE — FAILED (RT ENGINE)

RIGHT START VALVE OPEN LIGHT CAME ON IN FLIGHT, PASSING 16,000 FT ABOUT 10 MINUTES AFTER TAKEOFF. REMOVED AND REPLACED RIGHT ENGINE START VALVE IAW MD MM 80-10-02. OPS CHECKED GOOD IAW MD80 MM 71-00-00 AND 81-10-02 PAGE 204 THROUGH 207. (M)

Part: COALESCER BAG — DIRTY (A/C BAY)

MAIN ENTRY CABIN SERVICE REPORTED SMOKE/FUMES IN CABIN. REMOVED AND REPLACED COALESCER BAGS. ACCOMPLISHED PACK BURN PER 21-20-01-2. RAN BOTH ENGINES TO HIGH POWER. BOTH RIGHT AND LEFT PACKS OPS CHECKS NORMAL. (M)

Part: CABLE — LOOSE (SLIDE)

FORWARD GALLEY EXIT DOOR EMERGENCY SLIDE HAS A CABLE LOOSE ON THE GIRT BAR. RECONNECTED CABLE WIRED TO SLIDE, GOOD FOR SERVICE. (M)

Part: CABLE — LOOSE (SLIDE)

FORWARD GALLEY DOOR EMERGENCY SLIDE HAS A CABLE MECHANISM LOOSE AT BOTTOM OF SLIDE. RECONNECTED GIRT BAR CABLE ASSY TO DOOR SLIDE COVER. (M)

Part: SLIDE — DISLODGED (GALLEY DOOR)

LAX - EMERGENCY SLIDE AT FORWARD GALLEY IS FALLING OUT OF ITS CONTAINER. REINSTALLED SLIDE OK FOR SERVICE. (M)

Part: WIRE — BROKEN (WALKWAY)

RNO - EMPENNAGE O/H WALKWAY EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AND RELAMPED. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CCI-LAX - CEILING EMERGENCY LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED B5-104 BATTERY PACK. OPS NORMAL. (M)

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

SFO - RETURN TO SFO DUE TO NR 1 ENGINE COMPRESSOR STALL AT CLIMB POWER AT ABOUT 4,000 FEET. REDUCED POWER AND ENGINE RAN NORMAL EXCEPT FOR HIGHER EGT THAN RIGHT ENGINE FOR GIVEN EPR SETTING. REMOVED AND REPLACED NR 1 ENGINE PER QQ TASK CARD 0099. OPS AND LEAK CHECK GOOD. PERFORMED HI-POWER TRIM PER MM 71-00-00. ALL PARAMETERS MET. (X)

Part: SLIDE — DETACHED (GALLEY DOOR)

SEA - R1 DOOR ESCAPE SLIDE FELL OUT OF DOOR. RE-SECURED FORWARD GALLEY DOOR SLIDE AND COVER SLIDE CHECKS GOOD. (X)

Part: BATTERY PACK — DISCHARGED (EMPENNAGE)

SJC - EMERGENCY LIGHT AT EMPENNAGE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK LIGHT AT EMPENNAGE IAW MM 33-53-01. OPS CHECK GOOD. (M)

Part: FLOOR — CORRODED (CABIN)

OKC - LEVEL 2 CORROSION NR 5 FLOORBOARD PANEL AFT PIT IS CORRODED. FABBED NEW FLOOR PANEL FOR AFT PIT IAW DC9 SRM 51-10-2. OK TO TREAT. OK TO PRIME. REF: 10260 N/R 1000-0146. (X)

Part: FRAME — CORRODED (CARGO DOORWAY)

IN OKC, LEVEL 2 CORROSION AT MID PIT DOOR LOWER FRAME HAS CORROSION AT FORWARD AND AFT ENDS. REMOVED CORROSION FOUND FORWARD AREA OUT OF LIMITS REPAIRED IAW DC-9 SRM 53-05 FIG 63 TREATED AND PRIMED AREA IAW DC-9 SRM 51-10-2. REINSTALLED KICK PLATE FORWARD SECTION IAW DC-9 SRM 51-30-1 LEAK CHECK GOOD IAW MD-80 MM 21-32-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

IN RNO, OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED 'D' CELL NICAD BATTERIES IN CHARGER 35-27, OPS CHECK OF EMERGENCY LIGHT IS OK. (M)

Part: SENSOR — MALFUNCTIONED (TAIL COMP)

TAIL COMPARTMENT TEMP HIGH, LIGHT ILLUMINATED AFTER TAKEOFF. QRH PROCEDURE ACCOMPLISHED. LIGHT EXTINGUISHED. MAINTENANCE REMOVED SIDE PANELS. INSPECTED DUCTS WITH PACKS RUNNING. NO LEAKS NOTED. INSPECTED TEMP SENSOR AND AIR OUTLET. COULD NOT DUPLICATE AT THIS TIME. (M)

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHT OUT AT 15D. RECONNECT CANNON PLUG. OPS CHECK OK. (X)

Part: STEERING CYL — FAILED (NLG)

DURING TAXI, NOSE WHEEL STEERING FAILED RIGHT HYD SYSTEM PRESSURE AND QTY TO ZERO. REMOVED AND REPLACED LEFT NOSE WHEEL STEERING CYLINDER PER MM CHAP 32-52-02. (M)

Part: STARTER — FAILED (RT ENGINE)

RIGHT ENGINE WOULD NOT ROTATE. STARTER LIGHT ON. RETURN TO GATE. REPLACED STARTER, OPS OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (CARGO DOORWAY)

SSI INSPECTION REVEALED LEVEL 2 CORROSION ON AFT PIT DOOR FRAME ANGLE SUPPORT FITTING AT FWD LOWER DOOR OPENING. REMOVED AND REPLACED IAW DC-9 SRM 51-30. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (BS 1050)

SSI INSPECTION REVEALED LEVEL 2 CORROSION ON FRAME AT ZONE 7, STATION 1050. CORROSION OUT OF LIMITS. REPAIRED PER SRM 53-05 FIG 63. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (CARGO DOORWAY)

SSI INSPECTION REVEALED LEVEL 2 CORROSION AFT PIT DOOR FRAME AFT LOWER SUPPORT ANGLE. REMOVED AND REPLACED CORNER ANGLE IAW DC-9 SRM 51-10-2. INSTALLED IAW DC-9 SRM 51-30. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ANGLE — CORRODED (FWD LAV)

SSI INSPECTION REVEALED LEVEL 3 CORROSION AT FWD LAV THRESHOLD ANGLE. REMOVED DAMAGE ANGLE. FABRICATED NEW PART AND INSTALLED IAW DC-9 SRM 51-10-2 AND 51-30-2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — DISCONNECTED (CABIN)

STRIP ON EMERGENCY LIGHT MISSING IN REAR CABIN. FOUND EMERGENCY LIGHTING TERMINAL DISCONNECTED. RECONNECT STRIP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTORS — LOOSE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING INOPERABLE AT ROWS 10 AND 12. SEATED LOOSE CONNECTORS, OPS OK NOW. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD OVERWING EXIT LIGHTS OUT. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

AFTER TAKEOFF, CONTROL TOWER REPORTED SPARKS AND BLUE FLAMES OUT OF THE RIGHT ENGINE, ALL ENGINE INDICATIONS WERE UNEVENTFUL, TWO ENGINE LANDING WAS MADE. PERFORMED BOROSCOPE OF C-7 HI PRESSURE COMP SECTION FOUND L/E OF ALL BLADES. FOD'D ENTIRE LENGTH. REMOVED AND REPLACED NR 2 ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GENERATORS — MALFUNCTIONED (LT/RT)

STARTING TO TAXI, BOTH GENERATORS DROPPED OFF-LINE. MAINTENANCE PERFORMED BIT CHECK ON ALL GCU'S; RAN BOTH ENGINES; LOADED ALL SYSTEMS; UNABLE TO GET THE GENERATORS TO DROP. RAN ALL CHECKS IAW MM 24-20-01, PAGE 501. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

THREE SETS OF EMERGENCY OVERHEAD LIGHTS INOPERATIVE OVER AISLES 6, 7, 8, AND 9. REMOVED AND REPLACED WEAK BATTERIES. OPS CHECKS GOOD IN ROWS 6, 7, 8, AND 9. (X)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHTS AT ROWS 7-8-9 INOP (WIRE BROKEN AND BULB MISSING). REPAIRED WIRING AND RELAMPED. ALL FLOOR EMERGENCY PROXIMITY LIGHTING OPERATIONAL CHECKS OK. (M)

Part: BATTERY PACK — DISCHARGED

AFT EMERGENCY BATTERY PACK POWER SUPPLY INOP. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK POWER SUPPLY. OPS CHECK GOOD. (M)

Part: ATTACH PIN BOLT — SHEARED (LT MLG)

LEFT MLG LOWER TORQUE LINK ATTACH PIN BOLT SHEARED. REPLACED LT MLG LOWER TORQUE LINK ATTACH PIN BOLT IAW 32-17-01 DAC COMM. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

OVERHEAD 'CEILING' EMERGENCY LIGHT INOP, SEAT 6 THROUGH 10. REMOVED AND REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS SEAT 6 THROUGH 10. (M)

Part: EEL — INOP (CABIN)

EMERGENCY PORTABLE FLASH LIGHT AT FWD CABIN DOOR NOT PROPERLY WORKING. REMOVED AND REPLACED UNIT SYSTEM ARMS AND OPS NORMAL. (M)

Part: BOLT — BROKEN (NR 1 MAIN WHEEL)

NR 1 M/W ASSEMBLY, THROUGH BOLT SHEAR. REMOVED AND REPLACED NR 1 M/W ASSEMBLY DUE TO THROUGH BOLT SHEAR PER MM CHAP 32. (M)

Part: THRESHOLD — CORRODED (CARGO COMPT)

FORWARD PIT DOOR THRESHOLD CORRODED. TREATED AND PRIMED AREAS OF CORROSION. REMOVAL PER SRM 51-10-3. (X)

Part: ANTENNA — CORRODED (RADAR)

MINOR CORROSION ON FORWARD AND AFT FACE OF RADAR DISH. REMOVED CORROSION AND TREATED PER REFERENCE 51-10-3. (X)

Part: DRAIN DISK — MISSING (FWD GALLEY)

RETURN TO SJC, LOUD SQUEALING NOISE STILL PRESENT IN FWD GALLEY AREA. FOUND RESTRICTOR (AIR) MISSING IN FWD GALLEY WATER DRAIN LINES. INSTALLED RESTRICTOR. PRESSURIZED AIRCRAFT TO 4BSID. NO MORE SQUEAL. AIRCRAFT OK TO CONTINUE. (Z)