N457TM

Part: CIRCUIT BREAKER — FAILED (MLG INDICATOR)

GEAR DOWN LIGHTS FAILED. THE PILOT NOTICED HE DID NOT HAVE A LANDING GEAR DOWN INDICATION (3 GREEN LIGHTS) LANDING GEAR CHECK LIST HAD BEEN COMPLETED. WITH NO INDICATIONS THE TOWER WAS NOTIFIED THE PILOT ELECTED TO DO A GO AROUND AND ASK THE TOWER TO VERIFY THE GEAR WAS DOWN. THE TOWER ADVISED THAT HE COULD SEE ONLY THE NOSE WHEEL AND RIGHT MAIN GEAR DOWN. MAINTENANCE PEOPLE CAME OUT TO VERIFY IF THE LANDING GEAR WAS DOWN. THE PILOT ELECTED TO DO ANOTHER LOW PASS SO MAINTENANCE COULD VERIFY THE GEAR WAS DOWN. MECHANICS VERIFIED THE LANDING GEAR WAS DOWN, NORMAL LANDING WAS MADE WITH NO INCIDENT. RESET, CIRCUIT BREAKER CHECKED NORMAL ON GROUND. REQUESTED FLIGHT, ACCEPTANCE FLIGHT OK.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS)

DURING DESCENT NOTICED A SYS HYDRAULIC QUANTITY LEVEL DROPPING. A SYS LOW PRESSURE LIGHT ILLUMINATED. CONFIGURED AC FOR A SYS HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYS. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMINATED ON BOTH B SYS LOW PRESSURE WARNING LIGHTS, FLIGHT CREW OBSERVED A AND B PRESSURE INDICATION DROPPED TO ZERO AT THE SAME TIME, B SYS LOW QUANTITY DID NOT ILLUMINATE. CONFIGURED AC FOR MANUAL REVERSION, DIVERTED, MADE UNEVENTFUL LANDING. B SYS DID NOT LOSE FLUID. REPLACED HYDRAULIC TUBE ASSEMBLY TO 1 ENGINE DRIVEN HYDRAULIC PUMP ALSO CHANGED NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND THE MANIFOLD PRESSURIZATION REGULATOR, NO FURTHER DISCREPANCIES. AC RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — FAILED (A & B SYSTEM)

DURING DESCENT NOTICED A SYSTEM HYDRAULIC QUANTITY LEVEL DROPPING . A SYSTEM LOW PRESSURE LIGHT ILLUMINATED. CONFIGURED AC FOR A SYSTEM HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYSTEM. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMINATED ON BOTH B SYSTEM LOW PRESSURE WARNING LIGHTS, FLIGHT CREW OBSERVED A AND B PRESSURE INDICATION DROPPED TO ZERO AT THE SAME TIME B SYSTEM LOW QUANTITY DID NOT ILLUMINATE. CONFIGURED AC FOR MANUAL REVERSION, DIVERTED, MADE UNEVENTFUL LANDING.

Part: BATTERY PACK — DEFECTIVE (CABIN)

RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK CAUSES AN ELECTRIC DRAIN ON BATTERY WITH EMERGENCY LIGHT SWITCH OFF. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-33. OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

FOUND COCKPIT EMERGENCY LIGHT WOULD NOT TEST. REMOVE AND REPLACED EMERGENCY EXIT LIGHT IAW 33-51-51 OF BMM, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

R-3 OVERHEAD EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED R-3 EMERGENCY EXIT LIGHT IAW BMM 33-51-51. (M)

Part: CONNECTOR — DIRTY (T/E FLAP)

WING FLAP POSITION INDICATOR SHOWED FLAPS NOT RETRACTED THE LAST 5 DEGREES IN FLIGHT. FUNCTIONAL TEST OF FLAP RETRACTION AND EXTENSION SYSTEM BY MAINTENANCE OK. REMOVED FLAP POSITION INDICATOR TRANSMITTER ELECTRICAL CONNECTOR, CLEANED, INSPECTED AND RECONNECTED. REMOVED FLAP POSITION INDICATOR ELECTRICAL CONNECTOR, CLEANED, INSPECTED AND RECONNECTED. GROUND OPS CHECK NORMAL. (M)

Part: HYDRAULIC LINE

TOTAL HYDRAULIC FAILURE, FIRST NR 1 'A' SYSTEM PRESSURE LIGHT CAME ON, 'A' SYSTEM QUANTITY WENT TO ZERO. APPROXIMATELY 2 MINUTES LATER 'B' SYSTEM LOW QUANTITY LIGHT CAME ON. DIVERTED INTO SALT LAKE CITY, UT. INSPECTION FOUND BROKEN 'A' SYSTEM PRESSURE LINE AT PRESSURE MODULE. INSTALLED TEMPORARY FLEX LINE, OPS CHECK NORMAL, LEAK CHECK NORMAL IAW BMM 20-10-52, TO BE REINSPECTED AT PHASE CHECK. REVEALED 'B' SYSTEM BLEEDS TO 'A' SYSTEM. A/C RELEASED FOR FERRY FLIGHT, A/C IS SAFE FOR INTENDED FLT SLC TO EKO OPENED DMI TLD NR 0603, FOR TEMP FLEX LINE. UPON INVESTIGATION OF PROBLEM FOUND RUDDER PCU RETURN LINES SWAPPED IN TAIL SECTION, CORRECTED PROBLEM IAW 27-21-91. FOUND ELEVATOR FEEL ACTUATOR A/B RETURN LI

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND LEFT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHECK NORMAL. (M)

Part: HYDRAULIC LINE

LOST BOTH A/B HYDRAULIC SYSTEM PRESSURE. INSPECTED A/C FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC LINE FAILURE AT PRESSURE MODULE. A/C IS SAFE FOR ITS INTENDED FERRY FLIGHT WITH THE NR 1 ENGINE 'A' PUMP IN THE OFF POSITION. INSTALLED APPROVED RATED TEMPORARY FLEX HOSE OPS CHECK, LEAK CHECK, NORMAL IAW BMM 20-10-52. A/C RELEASED PER DMI TLD 0503, TLD NR 4570282-1, ITEM TRANSFERRED TO MASTER DMI LOG. REMOVED TEMP FLEX LINE AND INSTALLED HARD LINE PER BMM 20-10-51, LEAK AND OPS CHECK OK. 'A' SYSTEM AND 'B' SYSTEM RETURN LINES ON RUDDER PCU FOUND REVERSED. RETURNED 'A' AND 'B' RETURN LINES TO THE CORRECT POSITION, IAW DIAGRAM ON 27-21-91, PAGE 404, OPS AND LEAK CHECK NORMAL. NO LEAKS FOUND. AN INVESTIGATION IN

Part: LIGHT — INOPERATIVE (CABIN)

L1 EMERGENCY EXIT OVER DOOR LIGHT INOPERATIVE. RELAMPED PER BMM 33-51-101, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ROW 5 SEAT EMERGENCY LIGHT INOPERATIVE. RESEATED LAMP IN SOCKET, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FOUND RIGHT LOWER EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER BMM 33-51-21. OPS CHECK NORMAL. (M)

Part: BATTERY — INOPERATIVE (CABIN)

FOUND LEFT ROW 1 THROUGH 6 SEATS, INOPERTIVE EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT PER BMM 33-51-11, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FOUND ROW 12 AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AISLE, OPS CHECK NORMAL IAW BMM 33-51-11. (M)

Part: STRUT — LEAKING (NLG)

NOSE LANDING GEAR SHOCK STRUT LEAKING. REMOVED AND REPLACED NOSE LANDING GEAR STRUT ASSEMBLY PER B737 MM 32-21-0. (M)

Part: LIGHT — LOOSE (CABIN)

FOUND SEAT 21B EMERGENCY EXIT AISLE LIGHT LOOSE FROM SEAT. REATTACHED EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW BMM 33-51-11B. (M)

Part: LIGHT — LOOSE (CABIN)

SEAT 21 EMERGENCY LIGHT ASSEMBLY IS LOOSE FROM MOUNT. RE-ATTACHED LIGHT ASSEMBLY.

Part: HYDRAULIC LINE — CHAFED (ACTUATOR)

AT 31,000FT THE, B, LOW QUANTITY LIGHT ILLUMINATED IN FLIGHT, SYSTEM QUANTITY SHOWED 1.25 GALLONS, PILOT PERFORMED THE QRH FOR LOSS OF, B, SYSTEM HYDRAULICS, AND DIVERTED TO CEDAR RAPIDS IOWA.FOUND PRESSURE LINE NR6 SPOILER CHAFFED THRU, REPLACED HARD LINE WITH COMPATABLE FLEX HOSE. SERVICED HYDRAULICS LEAK AND OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD OVERHEAD CENTER EMERGENCY LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY.

Part: SEAL — BROKEN (ENG HYD PUMP)

NR 1 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. SYSTEM QUANTITY SHOWED 1-3 GALLONS. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, IAW BMM 29-11-31. OPS CHECK AND LEAK CHECK GOOD, IAW BMM 29-11-31. (M)

Part: ADC — INOPERATIVE (COCKPIT)

MODE C, 1 AND 2 INOPERATIVE BY 3,000 TO 4,000 FEET. RETURNED TO POINT OF ORIGIN. REMOVED AND REPLACED ADC, OPS CHECK GOOD, IAW BMM 34-12-11. (M)

Part: LIGHT — INOPERATIVE (CABIN)

R2 DOOR EMERGENCY EXIT OVER DOOR LAMP INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY IAW 33-51-101. (M)

Part: ENGINE — MALFUNCTIONED (NR 1)

DURING FLIGHT FROM COS PILOT NOTICED ENGINE OIL LEVEL GETTING LOW. OIL LEVEL CONTINUED TO DECREASE AND LOW LEVEL LIGHT STARTED TO ILLUMINATE. PILOT DECIDED TO SHUTDOWN NR 1 ENGINE 15 MINUTES OUT OF LAS. PILOT DECLARED EMERGENCY, AND LANDED SAFELY AT LAS. PEFORMED TESTS AND INSPECTION IAW PWA MM 72-00, EXCESSIVE OIL CONSUMPTION. INSPECT OIL PUMP AND SCAVENGE PUMP. CHECKED MAIN OIL SCREEN, ALL OK. PERFORMED BREATHER PRESS CHECK PER PWA MM 72-00, WITHIN LIMITS. NO EXTERNAL LEAKS FOUND. REMOVED AND REPLACED WITH SERVICEABLE ENGINE.(M)

Part: SKIN — CRACKED (FUSELAGE)

ON WALK AROUND, FOUND CRACKS ABOVE FORWARD WING TO BODY FAIRING AFT OF WING ILLUMINATION LIGHT OF LEFT WING IN FUSELAGE. REMOVED PAINT NDT VERIFIED 8 EACH CRACKS AT 8 RIVETS. REMOVED DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-30-3. (M)

Part: BULB — FAILED (CAIBN)

TWO NON ADJACENT AISLE LIGHTING FIXTURES INOPERATIVE. AIRCRAFT RELEASED PER MEL 33-19, DMI NR 0321 ITEM TRANSFER TO DMI LOG NR 518687394. REMOVED AND REPLACED EMERGENCY LIGHT FIXTURE BULBS. OPS CHECK GOOD IAW BMM 33-51-11. (M)

Part: BLADE — DAMAGED (NR 2 ENGINE)

NR 2 ENGINE FLAMED OUT ON TAKEOFF ROLL. INSPECTION OF ENGINE DETERMINE CAUSE TO BE INGESTION OF FOD, DAMAGING C-1, C-7, C-8 AND C-9 COMPRESSOR BLADES. (M)

Part: LINE — FAILED (HYDRAULIC SYSTEM)

'A' SYSTEM HYDRAULIC FAILED, LACK OF HYDRAULIC PRESSURE. REPLACED HYDRAULIC LINE LEFT WING T/E, PERFORMED LEAK CHECK OF BOTH ENGINES AND IN WHEEL WELL, NO LEAKS FOUND. REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP DUE TO CAVITATION. (M)

Part: PANEL — DELAMINATED (HORIZONTAL STAB)

UPON (PHASE 9) INSPECTION DISCOVERED RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL DELAMINATING. REPAIRED HORIZONTAL 1E PANEL WORK ORDER 02-0001, AND 02-0002, JOB NR 10-1166, WORK PERFORMED BY EVERGREEN AIR CENTER. (M)

Part: LIGHT — INOPERATIVE (SEAT 10C)

EMERGENCY LIGHT ON PASSENGER SEAT 10C IS BROKEN. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER BMM 33-51-11. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK ON RIGHT ENTRY DOOR PER BMM 33-51-71. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

EMERGENCY EXIT LIGHT ABOVE L-2 DOOR INOP. REPLACED EMERGENCY LIGHT ASSY IAW BMM 33-51-101, GROUND CHECKS NORMAL. (M)

Part: SENSOR — MALFUNCTIONED (APU COMPARTMENT)

LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RELEASED PER MEL 26-12, DMI 701, ITEM TRANSFERRED TO DMI LOG AND PLACARDED. REF: DMI 701, REMOVED AND REPLACED OVERHEAT LOOP IN APU COMPARTMENT IAW 26-18. OPS CHECKS NORMAL. (LOG PAGE 10721). (X)

Part: INSULATOR — MISLOCATED (APU)

ON GROUND LEFT WING BODY OVERHEAT ILLUMINATED. IN THE APU COMPARTMENT, THE OVERHEAT LOOP ELEMENT IS POSITIONED A FEW INCHES ABOVE THE BLEED AIR SUPPLY DUCT. THIS ELEMENT IS HELD IN POSITION BY NUMEROUS CLAMPS WITH INSULATORS DURING TROUBLESHOOTING, AN INSULATOR WAS FOUND TO BE POSITIONED AS TO WHERE THE ELEMENT WOULD INTERMITTENTLY GIVE A FALSE WARNING DUE TO THE TRANSFER OF HEAT FROM THE SUPPLY DUCT TO THE ELEMENT. THIS OVERHEAT PROBLEM WAS CORRECTED WHEN THE CLAMP INSULATOR WAS REPOSITIONED. (M)

Part: DETECTOR — OUT OF POSITION (APU)

NR 1 WING BODY OVERHEAT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT BFF WITH BLEEDS OFF, APU ON TAKEOFF, REMAINED OFF AFTER BLEEDS RECONFIGURED. DISCOVERED OVERHEAT DETECTOR AGAINST APU BLEED SUPPLY DUCT, RELOCATED AND RAN APU AT MAX TEMP FOR 40 MIN, NO DISCREPANCIES NOTED IAW BMM 49-11-0. (M)

Part: OVERHEAT LIGHT — ILLUMINATED (LT WING/BODY)

LEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING THE DESCENT INTO KEKO. AIRCRAFT RELEASED PER MEL 26-12, DMI 10508, ITEM PLACARDED AND TRANSFERRED TO DMI LOG. (M)

Part: FIRE DETECTOR — MALFUNCTIONED (LT WING/BODY)

LEFT WING BODY OVERHEAT ILLUMINATES, QRH PROCEDURE, LIGHT WENT OUT THEN CONTINUED FLICKERING DURING DESCENT. CHECKED ALL LOOPS WITH OHM METER AND MAGER, FOUND NO PROBLEM CHANGED FIRE DETECT ASSY UNIT TEST FLEW AIRCRAFT COULD NOT DUPLICATE PROBLEM. (M)

Part: CLAMP — LOOSE (LT WING/BODY)

LEFT WING BODY OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURE AND AFTER A FEW MOMENTS THE OVERHEAT LIGHT WENT OUT. RETORQUED CLAMP ON INBOARD END OF AIR CLEANER AT FORWARD END OF LEFT A/C BAY PER BMM 36-19-11, GRUOND CHECKS NORMAL. (M)

Part: CONNECTOR — DIRTY (LT WING/BODY)

LEFT WING BODY OVERHEAT ILLUMINATES INTERMITTENTLY. CLEANED CONNECTORS ON FORWARD AND AFT KEEL BEAM SENSOR, OPS CHECK NORMAL. OK FOR SERVICE. (M)

Part: CONNECTOR — DIRTY (LT WING/BODY)

LEFT WING BODY OVERHEAT LIGHT CAME ON DURING DESCENT. CLEANED CONNECTORS OF SENSING ELEMENT ON LEFT ENGINE STRUT CAVITY TESTED WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM PER BMM 26-18-0, PAGE 501, TO 502, TEST OK. (M)

Part: OVERHEAT LIGHT — ILLUMINATED (LT WING/BODY)

LEFT WING BODY OVERHEAT LIGHT CAME ON EN ROUTE. REMOVED AND REPLACED COMP OVERHEAT UNIT PER BMM 26-17-0, OPS TEST PERFORMED PER BMM 26-18-0, TEST OK. (M)

Part: CONNECTOR — FAILED (ENGINE)

ENGINE OVERHEAT LIGHT FLICKERED ON AND OFF. REMOVED AND REPLACED CONNECTOR PER BSWM 20-67-14, OPS CHECK NORMAL PER BMM 26-11-0. (M)

Part: FIRE LOOP — CHAFED (LT ENGINE)

LEFT ENGINE OVERHEAT LIGHT COMES ON INTERMITTENTLY. DISCOVERED CHAFED WIRES ON FIRE LOOP CONNECTORS, LT ENGINE, AFT. REMOVED AND REPLACED CONNECTORS PER BSWPM 20-62-16, OPS CHECKS NORMAL. (X)

Part: CONNECTORS — DIRTY (NR 1 ENGINE)

NR 1 ENGINE OVERHEAT LIGHT ON. CLEANED OVERHEAT LOOP CONNECTORS, REPLACED COPPER GASKETS. OPS CHECKED OK, IAW BMM 26-10-00. (M)

Part: CONTROL MODULE — DEFECTIVE (NR 1 ENGINE)

NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN-FLIGHT INTERMITTENTLY. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL MODULE, RAN ENGINE, NO LEAKS FOUND. CHECKED WIRING, ALL OK. REF MM 26-21-41, AND 26-21-0. (X)

Part: FIRE DETECTOR — DEFECTIVE (LT ENGINE)

LEFT ENGINE OVERHEAT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION ACCESSORY UNIT PER bMM20-10-111, GROUND TEST NORMAL PER BMM 26-11-0. (EKO) (X).

Part: CONNECTOR — DIRTY (NR 1 ENGINE)

SLT - NR 1 ENGINE OVERHEAT LIGHT IS ON INTERMITTENT IN FLIGHT, ON 100 PERCENT ON GROUND. AIRCRAFT RELEASED PER MEL 26-2, DMI 0402, PER PLACARD INSTALLED. CLEANED OIL FROM CONNECTORS ON NR 1 ENGINE PER BMM 26-11-0. TESTS NORMAL PER BMM 26-11-0. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

L2 DOOR EMERGENCY SLIDE BATTERY WEAK. REMOVE AND REPLACE BATTERY PACK PER BMM 33-51-71, GROUND CHECKS NORMAL. (M)

Part: SNUBBER — MISINSTALLED (PAX DOOR)

AIR LEAK IN L1 DOOR, GROUND PRESSURIZED AIRCRAFT. FOUND LOWER DOOR HINGE SNUBBER INSTALLED BACKWARDS. REPOSITIONED SNUBBER IAW BOEING MM CHAPTER 52-11-0 PAGE 406. REPLACED FLAPPER SEAL IAW STANDARD PRACTICES. OPS NORMAL. (M)

Part: FIRE LOOP — CHAFED (NR 2 ENGINE)

NR 2 ENGINE FIRE WARNING SYSTEM INTERMITTENT LIGHT AND BELL, 3 SECONDS IN LENGTH IN CRUISE AND APPROACH EKO. REPAIRED CHAFED WIRE FOR UPPER LOOP AT STATIONARY COWL FORWARD SUPPORT PER BSWP MANUAL, 20-00-11. GROUND CHECKS NORMAL. RAN ENGINE, NO PNEUMATICS LEAKS. (M)

Part: CONNECTOR — LOOSE (NR 2 FIRE DET)

FIRE WARNING ENGINE NR 2 LIGHT AND BELL ALARM. DISCOVERED LOOSE AND WATER SOAKED CONNECTOR ON ENGINE NR 2, FIRE DETECTION LOOP. CLEANED CONNECTOR AND TIGHTENED PER BMM 26-11-0. OPS CHECK NORMAL. (M)

Part: FIRE DETECTOR — FAILED (FUSELAGE)

APU FIRE DETECTION SYSTEM INOPERABLE. REMOVED AND REPLACED APU FIRE DETECTION ELEMENT PER BMM 26-15-11. OPS CHECK GOOD. (X)

Part: HANDLE — CRACKED (LT EMER EXIT)

LEFT EMERGENCY EXIT DOOR UPPER HANDLE CRACKED. REMOVED AND REPLACED LEFT EMERGENCY EXIT DOOR UPPER HANDLE PER BMM 52-21-0. (M)

Part: HANDLE — CRACKED (RT EMER EXIT)

RIGHT EMERGENCY EXIT DOOR UPPER HANDLE CRACKED. REMOVED AND REPLACED RIGHT EMERGENCY EXIT DOOR UPPR HANDLE PER BMM 52-21-0. (M)

Part: BATTERY — DISCHARGED (CABIN)

L2 DOOR EMERGECY LIGHT VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PER BMM 33-51-41. GROUND CHECKS NORMAL. (M)

Part: COVER — MISSING (CABIN)

EMERGENCY EXIT LIGHT COVER MISSING ON SIDEWALL AT ROW 10 ABC. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER ASSEMBLY PER BS WPM. OPS CHECK GOOD. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FORWARD SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPAIRED POWER SUPPLY POWER BMM 33-51-51. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

L-1 DOOR SLIDE EMERGENCY LIGHT BATTERY LOW VOLTAGE. REPLACED BATTERY PACK L-1 DOOR SLIDE PER BMM. TESTS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

L-2 DOOR SLIDE EMERGENCY LIGHT BATTERY LOW VOLTAGE. REPLACED BATTERY PACK L-2 DOOR SLIDE PER BMM. TESTS NORMAL. (M)

Part: BRAKE — DAMAGED (LT MLG)

LEFT LANDING GEAR CHATTERING. FOUND NR 2 BRAKE ASSY DAMAGED. REMOVED AND REPLACED NR 2 BRAKE ASSY PER 32-45-41. (X)

Part: WHEEL — DAMAGED (LT MLG)

LEFT LANDING GEAR CHATTERING. UPON INSPECTION, FOUND NR 2 MAIN WHEEL ASSY DAMAGED. REMOVED AND REPLACED NR 2 WHEEL ASSY EPR BMM 32-45-11. (X)

Part: WIRE — BROKEN (CABIN)

ROW 10 A, B, C, EMERGENCY EXIT WIRING BROKEN. SPLICED WIRES PE BSWPM. OPS CHECK GOOD. (M)

Part: BLEED VALVE — INOPERATIVE (NR 2 ENGINE)

LOSS OF CABIN PRESSURE, UNABLE TO MAINTAIN ALTITUDE IN MANUAL MODE. DEPLOYED OXYGEN MASKS. FOUND NR 2 ENGINE BLEED VALVE STUCK IN THE CLOSED POSITION. REMOVED AND REPLACED VALVE IAW BOEING MM 36-11-11. (M)

Part: TRIM TAB — LOOSE SCREWS (RT ELEV TRIM TAB)

PRECAUTIONARY LANDING AT OMA FOR IN FLIGHT VIBRATION. FOUND LOOSE SCREWS RIGHT ELEVATOR TRIM TAB P/N 657379945 SECURED SCREWS PER CASINO EXPRESS MM REFERENCE 27-31-31. AIRCRAFT RELEASED BACK TO SERVICE. INSPECTED WORK IN EKO OF LOOSE SCREWS, INSTALLATION CHECKS GOOD, PER BMM 27-31-31 ON ELEVATOR TRIM TAB. (M)

Part: MOUNT — CORRODED (NR 1 ENG)

DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE NR 1 ENGINE FORWARD MOUNTS MISSING SUPPAGE MARKS FOR ELASOMETRIC MATERIAL. REMOVED ISOLATORS, REMOVED CORROSION. SHOT PEENED AND REWORKED AREA. ULTRASONICALLY INSPECTED, APPLIED PRIMER, AND REINSTALLED ISOLATORS IAW B737 OHM 71-23-01 AND AERO CORP EO 96-396 REV IR DATED 11/19/96 WITH APPROVAL BY FAA FORM 8110-3. (M)

Part: SKIN — CRACKED (RT WING)

RIGHT WIND NR 4 SLAT INBOARD AUXILLARY TRACK CUT OUT, SKIN HAS .5 INCH LONG CRACK WBL 254. CUT OUT CRACKED FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737 SRM 57-30-4 AND 57-50-1 FIG 2. (M)

Part: SKIN — CRACKED (RT WING)

RIGHT WING NR 5 SLAT DE-ICE DUCT CUTOUT HAS .25 INCH LONG CRACK TOP CENTER. REMOVED CRACK FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-30-4 ND 57-50-3 FIG. (M)

Part: SKIN — CRACKED (WS 425)

RIGHT WING NR 4 SLAT AUXILLARY TRACK CUTOUT HAS .5 INCH LONG CRACK CENTER OF CUTOUT WSL 425. MECHANICALLY BLENDED CRACK EC VERIFIED NO FURTHER CRACKS. AFTER EVALUATION DETERMINED NOT TO BE ON SDR. (M)

Part: SPAR — CRACKED (RT TE MID FLAP)

UPON A SCHEDULED INSPECTION AT AERO CORP, THE LEFT INBOARD MID FLAP FRONT SPAR WAS FOUND WITH A GOUGE AND A 1.5 INCH CRACK AT THE NR 7 RIB FROM THE INBOARD END. (M)

Part: SEAT TRACK — CORRODED (BS 500-520)

DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL CORROSION WAS FOUND IN THE FORWARD CARGO COMPARTMENT AROUND FASTENER HOLES AND THE TIE DOWN PAD ON THE FLOR TRACKS AT FS 500B TO FS 520 STRINGER 27L. CUT OUT CORRODED SECTION OF TRACK. FABRICATED AND INSTALLED NEW SPLICE IAW B737 SRM 53-10-5 FIG 11, 51-10-1, 51-30-8, 51-20-4 AND 51-30-2. (M)

Part: RIB — CRACKED (LT TE FLAP)

DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD FLAP SECOND RIB FROM INBOARD END WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER. GAINED ACCESS TO AREA. REMOVED CRACKED RIB. DRILLED AND INSTALLED NEW RIB AND KIT IAW 737-200 SRM 51-10-02 PAGE 1, 51-10-01, 51-30-02, MM 27-51-01 AND 27-62-91. (M)

Part: RIB — CRACKED (LT TE MID FLAP)

DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD MID FLAP SIXTH RIB FROM INBOARD END WAS FOUND WITH TWO CRACKS ON THE LOWER FLANGE. REMOVED THE NR 6 RIB, CUT OUT GOUGED AND CRACKED SECTION OF WEB. FABRICATED AND INSTALLED TWO DOUBLERS AND FILLER. INSTALLED NEW RIB IAW B737 SRM 51-40-2, 51-30-02 PAGE 2,51-10-01, MM 51-21-31 AND AERO CORP EO 96-391 REV 1 DATED 11-11-96. (M)

Part: RIB — CRACKED (TE MID FLAP)

DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA THE LEFT WING INBOARD MID FLAP SEVENTH RIB FROM THE INBOARD END WAS FOUND WITH A CRACK ON THE LOWER FLANGE. REMOVED AND REPLACED WITH A NEW NR 7 RIB IAW B737 SRM 51-10-01, 51-30-02 PAGE 1 AND AERO CORP EO 96-391 REV 1 DATED NOV 13, 1996. (M)

Part: SPAR — CORRODED (LT TE MID FLAP)

DURIGN A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE LEFT WING INBD MID FLAP TRAILING EDGE WAS FOUND WITH DELAMINATION IN TWO PLACES 16 INCHES AT THE OUTBOARD EDGE AND 6 INCHES AT PREVIOUS REPAIR AT INBOARD EDGE. CUT OUT CORRODED HONEY COMB COMPOSITE AND REPLACED WITH NEW. CUT OUT CORRODED SECTION OF SPAR CHORD. FABRICATED AND INSTALLED REPAIR SECTION IAW AERO CORP FO 96-395 REV IR DATED 11/18/96. (M)

Part: FLOOR BEAM — CORRODED (BS 269)

DURING A SCHEDULED INSPECTION AT AERO COPR IN LAKE CITY, FLORIDA, THE LATERAL FLOOR SUPPORT ANGLE AT BS 268 BL 11L WAS FOUND WITH EXFOLIATED CORROSION ON THE UNDERSIDE OF THE FLT DECK. REMOVED CORRODED FLOOR BEAM. FABRICATED AND INSTALLED NEW FLOOR BEAM IAW B737 SRM 53-10-01 PAGE 1, 51-10-2, 51-41-161 AND 51-40-4. (M)

Part: C1/C2 DISK — LOOSE (ENGINE)

ON WALK AROUND INSPECTION, FOUND C1/C2 SPACER RETAINING NUT AND KEY WASHER INSIDE HUB ASSY. REMOVED ENGINE. (M)

Part: WIRE — BROKEN (CABIN)

ROWS 10 AND 15, EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AS REQUIRED. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EMERGENCY OVERWING EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IW MM 33-51-41. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

L2 DOOR EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED L2 DOOR EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. (X)

Part: SPLICE — FAILED (CABIN)

OVERWING SEAT EMERGENCY LIGHT LEFT, INOPERATIVE. REPAIRED SPLICE AND OPS CHECK OK IAW 20-30-12 AND 30-51-0. (X)

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS FORWARD BATTERY PACK LOW. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT BATTERY PACK PER BMM 33-51-51. OPS CHECK GOOD AT THIS STATION. (M)

Part: EEL BULB — FAILED (CABIN)

ROW 20 LEFT SIDE EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED MISSING EMERGENCY EXIT LIGHT IAW BSWP 20. OPSCHECKS GOOD THIS STATION. (M)

Part: SPOILER — REQUIRED ADJ (NR 7)

EKO - FLT 457 - AIRCRAFT ROLLED RIGHT 6 DEGREES AT 270 KIAS UPON INITIAL APP. OF SPEED BRAKE. ADJUSTED NR 7 SPOILER PANEL PER BMM 27-61-11.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT IAW BMM 33-51-31, OPS CHECKS OK. THIS CLEARS DMI NR 073. (X)

Part: EEL — INOPERATIVE (RT EXTERIOR)

RIGHT AFT EXTERIOR EXIT LIGHT INOP. REPLACED LIGHT IAW 33-51-21. OPS CHECKED OK AT THIS TIME. (X)