N317CM

Part: FIRE LOOP — FAULT MESSAGE (RT ENGINE) · airframe 113,784 hrs · 33,802 cycles

RIGHT ENGINE FIRE LOOP 2 STAUS MESSAGE, MTX GROUNDED A/C AND DEFERRED RT ENGINE FIRE LOOP 2 IAW MEL ABX-26-11-1-1. A/C REMAINS NO ETOPS . AND RETURNED A/C TO SERVICE.

Part: SPEED BRAKE — FAULTED · airframe 113,594 hrs · 33,701 cycles

DURING LANDING, AUTO DEPLOYMENT SPEED BRAKE ON THE GROUND INOP, NO LIGHTS OR EICAS MESSAGES. DEFERRED AUTO SPEEDBRAKE IAW MEL 27-62-1-1. CLEANED DEBRIS FROM SPEED BRAKE NO BACK CLUTCH ASSEMBLY. AUTO SPEED BRAKES CHECK GOOD PER B767 AMM 27-62-00. DI & PLACARD REMOVED. MTC PROCEDURES REVERSED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 2) · airframe 113,508 hrs · 33,664 cycles

SMELL OF FUMES. SMOKE IN CKPT 5 MILES OUT. LANDED, TOWER SAW SMOKE OUT OF #2 ENG ON TAXI. FIRE MASTER CAUTION CAME ON. SHUT #2 ENG DOWN, FIRE MASTER CAUTION WENT OUT. FIRE & SMOKE SEEN BY FIRE CREW. A/C CURRENTLY IN WORK. AN UPDATED SDR REPORT WILL BE FILED WHEN COMPLETED.

Part: BEAM — CORRODED (ZONE 600) · airframe 113,506 hrs · 33,663 cycles

THIS AIRCRAFT IS CURRENTLY UNDERGOING AN A-CHK IN CVG, AND MAINTENANCE FOUND THE RIGHT WING FIXED L/E NOSE BEAM AT OSS 500 TO BE BADLY CORRODED. THE CORROSION WAS REMOVED BY BLENDING, AND THE BLEND WAS BEYOND THE ALLOWABLE LIMIT GIVEN IN REF /A/. THERE IS NO REPAIR GIVEN FOR THIS DAMAGE IN THE B767-300 SRM SO FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /B/, WHICH IS AN FAA-DER APPROVED REPAIR. REPAIRED IAW FVCI EO 25185-3,AND ABX-REA-5740-65908-00.

Part: SKIN — CORRODED (ZONE 600) · airframe 113,506 hrs · 33,663 cycles

THIS AIRCRAFT IS CURRENTLY UNDERGOING AN A-CHK IN CVG, AND MAINTENANCE FOUND THE RIGHT WING UPPER T/E PANEL #1 AT WS 906 AFT OF REAR SPAR TO BE BULGED UP WHERE IT ATTACHES TO THE T/E OF THE WING SKIN. AFTER THE PANEL WAS REMOVED, CORROSION FOUND ON T/E OF WING SKIN PANEL #1 WHERE IT OVERHANGS REAR SPAR. CORROSION REMOVED BY BLENDING, & BLEND BEYOND THE ALLOWABLE LIMIT GIVEN IN REF A. THERE IS NO REPAIR GIVEN FOR THIS IN THE SRM SO FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF B, WHICH IS FAA-DER APPROVED REPAIR..REMOVED CORROSION & REPAIRED IAW FVCI EO 25185.2 REV IR W.S. 906, & ABX-REA-5725-65906-00.

Part: SKIN — CORRODED (ZONE 600) · airframe 113,506 hrs · 33,663 cycles

THIS AIRCRAFT IS CURRENTLY UNDERGOING AN A-CHK IN CVG, AND MAINTENANCE FOUND THE RIGHT WING UPPER T/E PANEL AT W.STA 433 TO BE BULGED UP WHERE IT ATTACHES TO THE T/E OF THE WING SKIN. AFTER THE PANEL WAS REMOVED, CORROSION WAS FOUND ON THE T/E OF WING SKIN PANEL #1 WHERE IT OVERHANGS THE REAR SPAR. THE CORROSION WAS REMOVED BY BLENDING, AND THE BLEND WAS BEYOND THE ALLOWABLE LIMIT GIVEN IN REF /A/. THERE IS NO REPAIR GIVEN FOR THIS IN THE B767-300 SRM SO FLIGHT VEHICLES CONSULTING, INC. WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /B/, WHICH IS AN FAA-DER APPROVED REPAIR. REMOVED CORROSION AND REPAIRED IAW FVCI EO# 25185-1 REV IR W.S. 433 PER ABX-REA-5725-65905-00.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 113,494 hrs · 33,653 cycles

DURING SERVICE CHECK FOUND FLIGHT DECK EMERGENCY LIGHT L9803 (IN CEILING, ACROSS FROM EXIT SIGN) INOP FOUND BATTERY ON PWR SUPPLY M736 FAULTY. REPLACED AND OPS CK GOOD AIW B767 AMM SUPPLEMENTAL 33-51-00 RURNED TO SERVICE

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 113,494 hrs · 33,653 cycles

DURING SERVICE CHECK FOUND FLIGHT DECK EMERGENCY LIGHT L9801 (BACK LEFT) INOP RELAMP NO HELP. "M736 BATTERY FAULTY" REPLACED BATTERY ASSY IAW B767 AMM SUPPLEMENTAL 33-51-00 OPS CK GOOD.RETURNED TO SERVICE.

Part: LIFE VEST — EXPIRED (ZONE 200) · airframe 113,487 hrs · 33,648 cycles

DURING SERVICE CHECK FOUND OBSERVER'S SEAT LIFE VEST INSPECTION DUE 09/01/2025. REMOVED AND REPLACED LIFE VEST IAW 25-62-00, SPEISIAL FREIGHTER SUPP. RETURNED TO SERVICE

Part: MODULE — DEFECTIVE (ZONE 300) · airframe 113,069 hrs · 33,448 cycles

ON TAXI OUT, RUDDER RATIO LIGHT ILLUMINATED AFTER ENGINE START AND WOULD NOT EXTINGUISH. A/C RETURNED TO BLOCKS (BTB). VERIFIED SHUTOFF, SERVO, AND LVDT WIRING. FOUND MODULE FAULT BALL ON LEFT UNIT. REMOVED AND REPLACED THE LEFT RUDDER RATIO MODULE, REF. B767 AMM 27-21-00. ALL FUNCTIONS AND INDICATIONS NORMAL. A/C RETURNED TO SERVICE.

Part: DOOR — UNLOCKED (ZONE 800) · airframe 112,972 hrs · 33,405 cycles

AFTER PUSHBACK DURING TAXI AND ENGINE START, PLANE CAME BACK TO GATE (BTB) DUE TO "MAIN CARGO DOOR" LIGHT ILLUMINATED. DURING CHECK, FOUND MAIN CARGO DOOR VENT WINDOWS OPENED AND "DOOR NOT LOCKED" LIGHT ON AT THE GALLEY PANEL. CYCLED MAIN CARGO DOOR IAW AMM 52-32-00. NO FAULTS OR DEFECTS NOTED. ALL CHECKS OK.MTX RETURNED A/C TO SERVICE

Part: CONTROL CABLE — DIRTY (AILERONS) · airframe 112,780 hrs · 33,312 cycles

DURING TAXI CREW PERFORMED FLIGHT CONTROL CHECKS AND REPORTED FLIGHT CONTROLS BINDING WHEN TURNING YOKE TO THE LEFT , SAME WITH FLAPS 0+5. AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC .PERFORMED GVI OF INBOARD AND OUTBOARD AILERON AND COMPONENTS. ALL LOOK SERVICEABLE, PERFORMED OPS CK FELT SLIGHT RESISTANCE AT END OF TRAVEL TO LEFT, CHECKED BUSHINGS ON ROD END OF COMPONENT FWD TO LOGPAGE 38723-44 BUSING GOOD, PERFORM SERVO TEST 07, TEST PASSED, UPON T/S FOUND DIRTY AILERON CABLE. CLEANED LUBED CABLES A/A-1, A/B-1, A/A-2, A/A-3, A/B-3 AND PULLEYS, CHECKED CABLE TENSION OF CABLE A/A-1, A/B-1, A/A-2, A/A-3, A/B-3, A/A-4, A/B-4, AB3A-1, AB3B-1, A3B-1, A3A-1, AB2B-1. AB2A-1, AB2A-2, AB2A-2, AB3A-2, AB3B-2. A4B-3, A4A-2, A4A-4, A4B-4, A3A-4, A3B-4, A3B-3, A3A-3 ALL CABLE TENSION GOOD. INSTALLED RIG PINS A-1, A-2, A4, A5, A6, A3, A-11, A-12, A-10, A19, A-9, A-15. RIG CK GOOD IAW B767 AMM 27-11-00, B767 SSM 27-10-01. CONTROL WHEEL MOVES SMOOTHLY.

Part: VALVE — FAULTED (NR 1 ENGINE) · airframe 112,308 hrs · 33,138 cycles

ON PUSHBACK #2 ENGINE STARTED NORMALLY. DURING ATTEMPTED START OF #1 ENGINE, N1 REACHED 26%,N2 FUEL CUTOFF SWITCHED MOVED TO "RUN", BUT ENGINE VALVE FAILED TO OPEN. GOT "L ENG FUEL" EICAS MESSAGE AND "ENG VALVE" DISCREET LIGHT ILLUMINATED. AC RETURNED TO GATE (BTB). AND MTX GROUNDED AC. MTX ACCOMPLISHED FIM 76-11 FAULT TREE 812 REPLACED 2 FUEL IGNITION CONTROL RELAY K168 OPS CHECK NORMAL IAW WDM 76-11-11 AND 71-00-00 A/C REMAINS ETOPS 180.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 111,924 hrs · 32,863 cycles

AFTER TAKE OFF, AND CLEANED UP CLIMBING THROUGH 4000'  AIRCRAFT HAD MODERATE AIRFRAME VIBRATION ON ENTIRE FUSELAGE. VIBRATIONS ON ENGINES WERE .9 (L) AND 1.5(R). CAME BACK TO CVG TO LAND - APPEARED NORMAL - TRIED TO GO TO MIA AND VIBRATION CAME BACK. RETURNED TO CVG MTX FOUND RIGHT ENGINE FAN (N1) LOCKED UP AND METAL IN TAILPIPE. RIGHT ENGINE REQUIRES REPALCEMENT.AC IS AOG UNTILL ENGINE CHANGE SEE L/P 38920-02/2. A/C RELEASED. NO ETOPS.

Part: VALVE — WARNING MESSAGE (LT HMG) · airframe 111,890 hrs · 32,849 cycles

LEFT HMG VAL STATUS MSG AFTER BLOCK OUT AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC RIGHT HMG PREVIOUSLY DEFERRED IAW ABX-24-25-2-1F, FOLLOWED DEACTIVATION PROCEDURES IAW AMM 24-00-00, REMAINS ETOPS 180. STATUS MESSAGE CLEARED.RETURNED AC TO SERVICE . AND AC DEPARTED

Part: UNKNOWN — VIBRATION · airframe 111,825 hrs · 32,818 cycles

AT LEVEL OFF FL290 HEARD A POP UNDER OUR FEET FOLLOWED BY NOTICEABLE VIBRATION.

Part: INDICATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 111,772 hrs · 32,790 cycles

ON TAXI OUT RUDDER TRIM FAILED TO MOVE TO THE RIGHT BUT MOVED TO THE LEFT . AC RETURNED TO BLOCK AND MAINTENANCE GROUNDED AC . TROUBLE SHOT AND CONFURMED RUDDER MOVEMENT, REMOVED AND REPLACED RUDDER TRIM INDICATOR IAW B767 AMM 27-28-05 OPS CHECK GOOD. MAINTENANCE RETURNED AC TO SERVICE AND DEPARTED

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 111,518 hrs · 32,683 cycles

RIGHT STARTER CUTOUT EICAS MESSAGE AND #2 ENG START VALVE LIGHT ILLUMINATED ON TAXI OUT. REMOVED AND REPLACED START CONTROL PANEL IAW B767 AMM 80-11-51. OPS CHECK GOOD, PLACARDS REMOVED. A/C VERIFIED NO ETOPS. NO MAINT PROCEDURES REQUIRED.

Part: WARNING MESSAGE — FALSE INDICATION · airframe 111,515 hrs · 32,681 cycles

IN FLIGHT RT ENGINE SHUTDOWN & RT ENGINE FUEL VALVE EICAS MESS. ENGINE RUNNING NORMAL, ALSO FALSE EGT EXCEEDANCE. AIRCRAFT IS AOG FOR TROUBLESHOOTING.

Part: WIRE — DAMAGED · airframe 111,515 hrs · 32,681 cycles

IN FLIGHT RT ENGINE SHUTDOWN & RT ENGINE FUEL VALVE EICAS MESS. ENGINE RUNNING NORMAL, ALSO FALSE EGT EXCEEDANCE. AIRCRAFT IS AOG. REMOVED W388-008-18 WIRE AND INSTALLED NEW WIRE FROM D4238P TO D4220J ALL PER B767 SWPM 20-10 REF B767 WDM 76-11-11. AC RETURNED TO NORMAL NO DEFECTS REF LOG PG 38595-90/1 FOR IDLE ENGINE RUN TO OBSERVE ENGINE INDICATIONS AC IS VERIFIED NO ETOPS.

Part: WARNING MESSAGE — ILLUMINATED (RT HYD SYSTEM) · airframe 89,570 hrs · 30,899 cycles

RT HYD QUANTITY LIGHT ON OVER HEAD, RT HYD EICAS MESSAGE (RT.00 RF) LIGHT. DEFERRED.

Part: CONTROL MODULE — FAULTY (RT ENGINE) · airframe 111,514 hrs · 32,680 cycles

APPROXIMATELY 25 MINS INTO FLIGHT THE EICAS DISPLAYED "R ENG SHUTDOWN" AND "R ENG FUEL VAL". IN-FLT START PARAMETERS WERE ALSO DISPLAYED. RIGHT "ENG VALVE" LIGHT ON CONTROL DISPLAYED CONTINUED PANEL. CONDUCTED T/S PER FIM 76-11 F.T. 813 R MEC REPLACEMENT REQUIRED. REPLACED R MEC PER AMM 73-21-01. A/C OK FOR SERVICE. A/C REMAINS NO ETOPS.

Part: RELAY — MALFUNCTIONED (RT ENG FUEL) · airframe 111,140 hrs · 32,521 cycles

DURING TAXI AFTER RIGHT ENGINE START, RIGHT ENGINE FUEL VALVE LIGHT AND "R ENG FUEL VAL" EICAS MESSAGE ILLUMINATED AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE DEFERRED ENGINE VALVE INDICATION IAW MEL ABX-73-21-3-1. RETURNED AC TO SERVICE AND DEPARTED.LIGHT + EICAS OPS NORMAL BEFORE TROUBLESHOOTING. REPLACED RELAY K169. VERIFIED BOTH IGNITIONS + FUEL DELIVERY, REF B767 AMM 76-11-00 ALL LIGHTS + EICAS INDICATIONS NORMAL. THIS CLEARS DI 48905. PLACARD REMOVED. NO REACTIVATION PROCEDURES REQUIRED. AIRCRAFT REMAINS "ETOPS 180".

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,680 hrs · 32,317 cycles

DURING TAXI AFT CABIN TEMP EICAS MSG. A/C RETURNED TO BLOCK GROUNDED BY MAINTENANCE DEFERRED SYSTEM IAW ABX- MEL 21-61-1-2. RETURNED AC TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 109,885 hrs · 32,009 cycles

DURING N317CM C-CHECK AT AIRBORNE (TAMPA), FWD CARGO COMP FLOOR BEAM UPPER CAP EXFOLIATED AT STA 701 LBL 48. REMOVED CORROSION IAW B767-300 SRM 51-00-02 ORIGINAL THICKNESS .100 REMOVED .030 REMAINING THICKNESS .070 TO BR OUT OF LIMITS IAW B767-300 SRM 53-00-07 INSTALLED FLOOR BEAM REPAIR IAW B767-300 SRM 53-00-07 REPAIR 4.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 109,885 hrs · 32,009 cycles

DURING N317CM C-CHECK AT AIRBORNE (TAMPA), THE FWD CARGO FLOOR SUPPORT BEAM (P/N 451T1604-2) AT STA 548, RBR 41.28 HAS CORROSION. THE DAMAGE WAS REMOVED BY BLEND-OUT PROCESS. THE FLOOR SUPPORT IS FABRICATED FROM 7075-T6511 AL ALLOY EXTRUSION (BAC1506-1898) PER QQ-A-200/11. THERE ARE NO REPAIRS FOR THE SPECIFIC LOCATION IN THE 767-300 SRM AND DUE TO UNDERLYING STRUCTURES, UNABLE TO PERFORM TYPICAL EXTRUDED SECTION REPAIR PER SRM 51-70-12. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. AAIRCRAFT WAS REPAIRED PER ABX-REA-5331-64861-00.

Part: SKIN — CRACKED (ZONE 100) · airframe 109,060 hrs · 31,734 cycles

DURING ROUTINE LINE MAINTENANCE IN CVG MAINTENANCE DISCOVERED SKIN CORRODED WITH EVIDENCE OF CRACK @ STA 1234 S37R. REPAIRED SKIN IAW B767 SRM 53-00-01 REPAIR 12. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (FUEL PUMP) · airframe 109,055 hrs · 31,729 cycles

CENTER LEFT FUEL PUMP EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED LEFT CTR. FUEL PUMP IAW MEL 28-22-2A. MAINT. PROCEDURES COMPLIED WITH. PLACARD INSTALLED. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER RATIO) · airframe 108,508 hrs · 31,545 cycles

RUDDER RATIO EICAS CAUTION MESSAGE DISPLAYED AFTER ENG START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED BFIM 27-21 FT 804, NO DEFECTS NOTED AT THIS TIME. STARTED BOTH ENGINES. RUDDER RATIO LIGHT EXTINGUISHED AS REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER) · airframe 108,507 hrs · 31,544 cycles

AFTER ENGINE START, RUDDER RATIO EICAS MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET FLT CONTROL ELEC CIRCUIT BREAKERS IAW B767 AMM 27-09-11 AND 20-60-05. MESAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — LEAKING (RIGHT) · airframe 108,484 hrs · 31,535 cycles

RT ENG DUCT PRESS FLUCTUATES WITH ENG RUNNING AND BLEED AIR SW ON. SECONDARY INDICATIONS ON CABIN ALT, RATE, AND DIFF GAGES. CREW ELECTED TO DIVERT INTO CVG. LANDING WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND R/H AIR CYCLE MACHINE HAS LEAK AT AIR BEARING HOUSING. REMOVED AND REPLACED R/H AIR CYCLE MACHINE IAW B767 AMM 21-51-03. OPS CHECK AND LEAK CHECK GOOD. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAULTED (ZONE 100) · airframe 108,478 hrs · 31,534 cycles

AFTER PUSH SHUT DOWN APU AND GOT AN APU FUEL VALVE LGT WITH FAULT LGT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED APU FUEL ACTUATOR IAW AMM 28-25-02 OPS CK NORMAL A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: FILTER — CONTAMINATED (RT ENG FUEL) · airframe 108,451 hrs · 31,527 cycles

R ENG FUEL FILT EICAS MESSAGE AFTER TAKEOFF CREW PERFORMED AIR TURN BACK TO CVG. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE CONDUCTED T/S PER FIM 73-11 FT 803 FOUND DEBRIS IN FUEL FILTER OF RT ENGINE REPLACED FUEL FILTER PER AMM 73-11-02, LEAK CHECK OK. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 107,835 hrs · 31,371 cycles

RUDDER RATIO EICAS MSG AFTER BLOCK OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET RUDDER RATIO MODULES AND TESTED RUDDER IAW B767 FIM 27-21 FT 804 OPS CHECKED GOOD NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SERVO VALVE — FAULTED (ZONE 300) · airframe 107,812 hrs · 31,360 cycles

RUDDER RATIO DISCRETE LIGHT ILLUMINATED AS WELL AS RUDDER RATIO EICAS MESSAGE ILLUMINATED AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED RUDDER RATIO CHANGER SERVO VALVE IAW AMM 27-21-15. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — FAULTY (ZONE 100) · airframe 107,810 hrs · 31,359 cycles

RUDDER RATIO EICAS MSG AFTER PUSH BACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.MAINTENANCE REMOVED + REPLACED R RUDDER RATIO MODULE IAW B767 AMM 27-11-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — OUT OF TOLERANCE (ZONE 100) · airframe 107,630 hrs · 31,313 cycles

FMC DROPPED WPT NAVIGATING TO ON CLIMB OUT RE ENTERED AND ACTIVATED ROUTE 2 WPT NAV DROPPED A SECOND TIME. CREW ELECTED TO PERFORNM AN AIR TURNBACK.AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND EXCESSIVE DRIFT FOR LEFT IRS. REPLACED THE LEFT IRS REF B767 AMM 34-21-00. VERIFIED PROPER IRS FUNCTION ALONG WITH FMS SYSTEMS, REF B767 AMM 34-61-00. AIRCRAFT RETURNED TO SERVICE

Part: NONE — NONE · airframe 107,569 hrs · 31,293 cycles

RADAR WOULD NOT TEST ON TAXI OUT. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED RADAR GROUND TEST, TEST NORMAL IAW B767 AMM 34-43-00. AIRCRAFT REMAINS ETOPS 180 OPERATIONAL. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (RIGHT ENGINE) · airframe 107,206 hrs · 31,191 cycles

RT ENG EEC INOP LIGHT ILLUMINATED WITH ASSOCIATED RT ENG EEC EICAS MESSAGE DISPLAYED DURING T.O. ROLL. ABORTED TAKE OFF AND AIRCRAFT RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT RT EEC SYSTEM. REMOVED OLD, THEN INSTALLED NEW R/H ELECTRICAL T.12 SENSOR PER AMM 73-21-06. TEST OF R/H SENSOR AND EEC OK PER AMM 73-21-07. CONDUCTED TEST 3, 4, 11 PER AMM 71-00-00/501, ALL TESTS PASSED. A/C REMAINS ETOPS 180, AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (ZONE 100) · airframe 107,154 hrs · 31,182 cycles

R GEN DRIVE DISC LIGHT UPON START UP TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE VERIFIED RIGHT ENGINE OIL SERVICING IAW B767 AMM 12-13-03, NO DEFECTS. REMOVED AND REPLACED RIGHT GCU IAW B767 AMM 24-22-07. BITE AND OPS CHECK GOOD. ACCOMPLISHED IDLE ENGINE RUN IAW B767 AMM 71-00-00. DRIVE LIGHT DID NOT ILLUMINATE WHEN APU SHUTDOWN. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE

Part: NOT REPORTED — NOT REPORTED · airframe 106,939 hrs · 31,118 cycles

DURING L ENGINE START, L ENG STARTER EICAS, WITH VALVE DISCRETE LIGHT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DRY MOTORED LEFT ENGINE. START VALVE OPS CHECKS NORMAL IAW B767 AMM 80-11-00. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 106,657 hrs · 31,050 cycles

L ENGINE STARTER EICAS ( HUNG START ). AIRCRAFT RETURNED TO BLOCKS AND GROUNDED BY MAINTENANCE. PERFORMED A MAINTNENANCE ENGINE RUN. ENGINE STARTED AND RAN NORMALLY. NO MESSAGES IAW AMM 71-00-00 AIRCRAFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 106,239 hrs · 30,897 cycles

AUTO THROTTLE AUTOMATICLLY DISENGAGED. FLIGHT CREW ELECTED TO REJECT TAKE OFF AT 40 KTS. AIRCRAFT RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED A/T SYSTEM PER MEL 22-30-1A. MAINTENANCE PROCEDURE C/W, PLACARD INSTALLED. A/C RALM DOWNGRADED TO CAT 1, AIRCRAFT RELEASED BACK IN SERVICE

Part: PIN — WORN (CARGO DOOR LATCH) · airframe 105,077 hrs · 30,576 cycles

DURING C-CHECK, MAIN CARGO DOOR LATCH PINS WERE FOUND TO BE WORN BEYOND LIMITS. REMOVED AND INSTALLED NEW CAM PINS AT MAIN CARGO DOOR IAW ABX 767 AMM 52-32-11 AMM.

Part: RELAY — INTERMITTENT (PITOT HEAT) · airframe 103,970 hrs · 30,217 cycles

AFTER BLOCK OUT DURING ENGINE START, PROBE HEAT EICAS MESSAGE ACCOMPANIED BY LT AUX PITOT AND F/O PITOT DISCREET LIGHTS ON OVERHEAD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED. REMOVED AND REPLACED RELAY K241, PER SWPM 20-81-00 REF WDM 30-31-11 AND MISC TEST PANEL PER B767 AMM 24-22-06. OPERATIONS NORMAL OF ALL PROBE HEAT SYSTEMS, PER B767 MM 30-31-00. A/C REMAINS RVSM COMPLIANT AND ETOPS 180. AIRCRAFT RELEASED.

Part: PROXIMITY SENSOR — WORN (SLAT SYSTEM) · airframe 103,431 hrs · 30,016 cycles

SLAT ASYM EICAS MESSAGE, AIRCRAFT RETURNED TO BLOCK AND GROUNDED. PERFORMED PSEU BITE TEST PER B767 FIM 32-09, FAULT TREE 803 AND FOUND CODE 286 (NR 5 INBOARD SLAT FAR). ACCOMPLISHED A DETAILED VISUAL INSPECTION ON L/E SLAT SYSTEM AND COMPONENTS AND FOUND NR 5 SLAT INBOARD PROX SENSOR AND TARGET DAMAGE. REMOVED AND REPLACED NR 5 SLAT INBOARD PROX SENSOR AND TARGET PER B767 AMM 27-88-01, OPS CHECK SATISFACTORY. NO EICAS MESSAGE AT THIS TIME.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 103,311 hrs · 29,967 cycles

AT FL 350 TAT-13, N1 FLUCTUATES BETWEEN 90.8- 92.4, EGT FLUCTUATES BETWEEN 657-668, N2 FLUCTUATES BETWEEN 95.6-97.0, FF AT 2.3, OIL PRESS 55, OIL TEMP 114,N2 VIB 0.8 (LT ENGINE READINGS). AIRCRAFT WAS GROUNDED AND LT ENG EEC DEFERRED, A/C RELEASED NO ETOPS MEL 73-21-1-1B.

Part: WIRE — CORRODED (AUTOPILOT SYS) · airframe 103,281 hrs · 29,952 cycles

MAINTENANCE WAS BEING PERFORMED ON AUTO PILOT SYSTEM FOR NO LAND 3 EICAS MESSAGE. RT AUTOPILOT WILL NOT ENGAGE. WIRING WAS FOUND TO BE CORRODED. WIRE W1729-002-20. AIRCRAFT WAS GROUNDED AND SPLICE REPAIR TO WIRING WAS COMPLETED.

Part: ENGINE — POWER LOSS (LEFT) · airframe 103,211 hrs · 29,932 cycles

ON CLIMB OUT LEFT ENGINE STARTED TO FLUX. AIRCRAFT WAS GROUNDED.

Part: WARNING MESSAGE — ILLUMINATED (RT BUSS ISOLAT) · airframe 103,144 hrs · 29,902 cycles

RIGHT BUSS ISOLATION MESSAGE IN FLIGHT. RIGHT IDG HIGH TEMP. AIRCRAFT WAS GROUNDED.

Part: GENERATOR — INOPERATIVE (RIGHT) · airframe 102,912 hrs · 29,830 cycles

ENGINE DRIVEN GEN SYSTEMS IDG,GCB GE-RIGHT GEN INOP EICAS MESSAGE RIGHT GEN DRIV. AIRCRAFT WAS GROUNDED.

Part: EICAS — MALFUNCTIONED (COCKPIT) · airframe 102,396 hrs · 29,613 cycles

EICAS DISPLAY UNIT, ABORT TAKE OFF DURING TAKE OFF ROLL AT APPROXIMATELY 80 KNOT. THE AIRCRAFT WAS GROUNDED.

Part: WIRE — CHAFED · airframe 101,833 hrs · 29,341 cycles

DURING TROUBLESHOOTING FOR THE APU BATTERY NOT CHARGING, THE CIRCUIT BREAKER, C302, WAS FOUND TRIPPED OPEN AND THREE WIRES W238-001-18, W238-002-18, W238-003-18 OVER THE CENTER TANK WERE FOUND CHAFED AND SHORTED TOGETHER. THE WIRES WERE REPAIRED AND THE BATTERY CHARGER OPERATIONALLY CHECKED GOOD. THE CAUSE OF THE WIRE CHAFING WAS A FOREIGN OBJECT LAYING ON THE WIRE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) DURING THE TROUBLESHOOTING AND REPAIR.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

DAMAGE ON THE CENTER WING BOX LOWER BEAM, LOWER CHORD BETWEEN FUSELAGE STATIONS 900 AND 925. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE FORWARD CARGO COMPARTMENT LOWER LOBE FUSELAGE FRAME WEB AT FUSELAGE STATION 654. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE MAIN LANDING GEAR WHEEL WELL FUSELAGE STATION 1065 BULKHEAD HORIZONTAL STIFFENER NR 4 BETWEEN LBL 65 TO RBL 25. THE STIFFENER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE LOWER FUSELAGE SPLICE PLATE AT FUSELAGE STATION 1087, STRINGER 36R. THE SPLICE PLATE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: PLUG — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON LEFT SIDE WINDOW PLUG AT FUSELAGE STATION 845. THE WINDOW PLUG WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CRACK IN THE FORWARD LOWER CARGO COMPARTMENT GILL LINER STRAP SUPPORT ANGLE AT FUSELAGE STATION 632. THE ANGLE CLIP WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE UPPER SURFACE OF THE FUSELAGE SKIN CIRCUMFERENTIAL SPLICE PLATE AT FUSELAGE STATION 434, STRINGERS 39L AND 39R. THE SPLICE PLATE WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE LOWER AFT CARGO COMPARTMENT FLOOR SUPPORT WEB AT FUSELAGE STATION 1263 - 1285. THE WEB WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: STRUCTURE — WORN (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

LOWER CHORD ABOVE LEFT AIR CONDITIONING PACK RAM AIR INLET WORN BEYOND LIMITS. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THREE DRAIN SUPPORTS AT FUSELAGE STATION 1605. THE DRAIN SUPPORTS WERE REPLACED. THE AIRPLANE WAS GROUNDED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD AT FUSELAGE STATION 500, STRINGER 34R. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN PANEL — DAMAGED (RT HORIZ STAB) · airframe 101,467 hrs · 29,176 cycles

RIGHT HORIZONTAL STABILIZER INTERNAL DAMAGE FROM FOREIGN OBJECT ON THE LOWER PANEL INNER SKIN AT AUXILIARY SPAR STATIONS 240 - 701. THE SKIN PANEL WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: PANEL — WORN (RT PYLON) · airframe 101,467 hrs · 29,176 cycles

RIGHT PYLON PANEL 447AL WORN BEYOND LIMITS. THE PANEL WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 101,467 hrs · 29,176 cycles

CORROSION ON THE FORWARD LOWER CARGO COMPARTMENT BALLMAT SUPPORT ASSEMBLY AT FUSELAGE STATION 588. THE SUPPORT ASSEMBLY WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CRACKED (BS 1197) · airframe 101,249 hrs · 29,082 cycles

CRACK IN THE FUSELAGE SKIN AT FUSELAGE STATION 1197+124, STRINGER 37L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: DOOR SILL — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON THE INNER SILL OF THE BULK CARGO DOOR FRAME BETWEEN BS 1395 AND 1417, STRINGER 33L, THE DOOR SILL WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1481-1560) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON FLOOR SUPPORT OF BULK CARGO FLOOR. THE SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1395) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON TOP OF FLOOR SUPPORT AT BS 1395. THE FLOOR SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: ROLLER TRAY — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON THE FLOOR ROLLER TRAY ASSEMBLY IN THE AFT LOWER CARGO COMPARTMENT AT STA 1417. THE ROLLER TRAY ASSEMBLY WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON RIGHT HORIZONTAL STABILIZER UPPER SKIN AT RIGHT HSS 52.5 BETWEEN RIBS 4 & 5. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: FILLER — CORRODED (BS 1536-1540) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON FILLER AT LEFT AFT ENTRY DOOR CUTOUT BETWEEN INNER DOUBLER AND SKIN. THE FILLER WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: DOOR FRAME — CORRODED (BS 1481) · corrosion level 2 · airframe 97,131 hrs · 27,334 cycles

CORROSION ON WEB OF THE BULK CARGO DOOR FRAME AT BS 1481, STRINGER 30L. THE WEB WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 92,974 hrs · 25,642 cycles

NUMBER 1 FLAP SUPPORT 1 - 3 BEAM HAS A HOLE WITH DEFECT INDICATION ON HFEC ROTARY SCAN, POSSIBLE PITTING. NR 1 FLAP SUPPORT 1 - 3 BEAM, RE-WORKED IAW REA CO57-61638-MR. CORRODED LEVEL 2, PN 113T1498-7, PART NAME 1 - 3 SUPPORT BEAM, SN ABXV885, FROM WS EXACT 798.2. ACFT WAS GNDED.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 92,974 hrs · 25,642 cycles

REA NO C057-61644 MR ISSUED, REAMED 3 EA HOLES ROUND & TRUE, COMPLIED WITH HFEC. ALL DEFECTS REMOVED IAW SRM 51-10-02 PARA 11. FOR DETAILS ALSO SEE WORK STEPS 1 - 17 OF REA FOR WORK PERFORMED. CORRODED LEVEL 2, PN 113T1499-12, PART NAME 1 - 3 BEAM NR 7 SUPPORT. SN ABXV947, EXACT WS WS 616 RT. ACFT WAS GNDED.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 92,974 hrs · 25,642 cycles

NUMBER 2 FLAP SUPPORT 1-3, BEAM HAS 3 HOLES ON INBD SIDE & 1 HOLE ON OTBD SIDE WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN. HOLES REPAIRED IAW REA C057-61643-MR. PN 113T1499-11, SN ABXV89U, PART NAME NR 2 FLAP SUPPORT 1 - 3 BEAM, CORRODED LEVEL 2, EXACT WS LOCATION ON ACFT WS 616 LT. ACFT WAS GNDED.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 92,974 hrs · 25,642 cycles

NUMBER 1 ENG AFT FAIRNG, MOST FWD FRAME STATION ALONG BOTTOM OF FAIRING ASSEMBLY IS CRACKED IN SEVERAL LOCATIONS , AS VIEWED FROM INBD SIDE OF FAIRING LOOKING FWD. R & R FRAME CHANNEL & B STIFFENER ANGLE AT NR 1 ENG AFT FAIRING MOST FWD FRAME IAW SRM 51-40-02 PARAGRAPH 7. CRACKED 2 INCHES, PN 313T2380-279, PART NAME OTBD STIFFENER & CHANNEL, SN FS & BS LOCATION EXACT NAC 308.37. ACFT WAS GNDED.

Part: SHAFT — CORRODED (TE FLAP) · corrosion level 2 · airframe 92,974 hrs · 25,642 cycles

REMOVED & REPLACED LT INBD FLAP 6 - 6 PIN IAW AMM 27-51-04-002-134 & 27-51-04-402-135. CORRODED LEVEL 2, PN 113T1216-1, PART NAME SHAFT ASSEMBLY, SN NSN & ACFT WAS GNDED.

Part: BRACKET — CORRODED (ZONE 400) · corrosion level 2 · airframe 92,974 hrs · 25,642 cycles

BRACKET FWD OF INBD HYD BAY DOOR AFT HINGE IS CORRODE. FOUND TO BE OUT OF LIMITS. R & R BRACKET IAW SRM 51-40-02 SEC C PG 9 FG 15. CORRODED LEVEL 2, PN 313T3310-147, PART NAME BRACKET, SN N/A, FS BS LOCATION NR 2 PYLON NAC STATION 366. ACFT WAS GNDED.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 92,974 hrs · 25,642 cycles

PANEL 437DB, OTBD ATTACH ANGLE CRACKED. R & R ATTACH ANGLE, CHANNEL, IAW SRM 51-40-02 PARAGRAPHS 4 & 7. CRACKED 3", PN 313T3360-79, PART NAME CHANNEL, SN NSN, EXACT FS FROM NAC STATION 421. ACFT WAS GNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,974 hrs · 25,642 cycles

CRACK FOUND ON LEFT STATION 883.5, SIDE FRAME INNER CHORD. REFERENCE NEA53000047-001. REPAIRED ON JC EA 53000049-201. CRACKED 1", PN 691T0003-45, PART NAME CHORD, SN NSN, EXACT FS 883.5, STRINGER & WS LOCATION LBL 89. ACFT WAS GNDED.

Part: MANIFOLD — CRACKED (LT ENGINE) · airframe 91,917 hrs · 25,246 cycles

LEFT ENG LOW PRESS TURBINE VIBRATION LEVEL AT 4.8 - 5.0 DURING FLIGHT. CRACKS FOUND ON THE ENGINE’S TURBINE CASE COOLING MANIFOLD. REPLACED LT ENG. CAUSE UNKNOWN AT THIS TIME. PENDING ENG SHOP FINDINGS.

Part: STRUT — CRACKED (LE SLAT) · airframe 89,711 hrs · 24,497 cycles

NUMBER 2 SLAT OTBD AUXILIARY TRACK ATTACH FITTING OTBD LOWER STRUT SPLIT ON EDGE. INSTALLED NEW LOWER STRUT IAW SRM 51-40-02 & REA NR B657-60825-MR. SDR INFO 1/2 INCH CRACK, PN 114T2224-15, PART NAME STRUT, SN NSN, LOC AT 0SS 937.929. ACFT WAS GROUNDED.

Part: SLAT — CORRODED (LE SLAT) · corrosion level 2 · airframe 89,711 hrs · 24,497 cycles

NUMBER 4 SLAT UPPER LE SKIN SURFACE CORRODED & BUBBLED. NR 4 SLAT CORRODED OUT OF LIMITS. R & R SLAT IAW AMM 27- 581-02, OPERATIONS CHECKED GOOD. SDR INFO LEVEL 2 CORROSION, PN 114T4104-53, PART NAME SLAT, SN 000742, LOC FROM LES 500 TO LES 690. ACFT WAS GROUNDED.

Part: BRACKET — CRACKED (LE SLAT) · airframe 89,711 hrs · 24,497 cycles

THREE ANGLE BRACKETS ON THE LOWER INTERIOR EDGE OF THE NR 6 SLAT ARE TWO EACH CRACKED & ONE EACH HAS LOOSE HARDWARE, APPROXIMATE STATION 281. R & R TWO EACH CRACKED BRACKETS & RE TORQUED LOOSE HARDWARE ON ONE EACH BRACKET ON NR 6 SLAT APPROXIMATE STATION OSS 281 IAW DWG 114T3162 & SRM 51-40-02. SDR INFO CRACK LENGTH 1 INCH, PN 114T66Y107, PART NAME BRACKET, SN NSN, LOC OSS 281. ACFT WAS GROUNDED.

Part: RETAINER — CRACKED (NR 1 NACELLE) · airframe 89,711 hrs · 24,497 cycles

NUMBER 1 INBD NACELLE AT HYD BAY HAS A CRACKED SEAL RETAINER IN THE MIDDLE AREA. R & R SEAL RETAINER IN THE MIDDLE SECTION OF NR 1 NACELLE HYD BAY DOOR IAW SRM 51-40-02, PAR 7, PG 4. SDR INFO CRACKED LENGTH 1, 1.5 INCHES PN 313J2380-269, SN NA, PART NAME SEAL RETAINER, LOCATION FROM NACELLE STATION 330 TO 350. ACFT WAS GROUNDED.

Part: DOOR — MISREPAIRED (ZONE 800) · airframe 85,577 hrs · 23,204 cycles

EXTERNAL DOUBLER EXISTING REPAIR AT STA 1439 TO 1461, STR 25 LT TO 27 LT NEEDS EVALUATED. R & R DOUBLER AND REPAIRED DAMAGE IAW REA B652-59860-MR, AND SRM 52-30-01 FIG 201.

Part: SKIN — MISREPAIRED · airframe 85,577 hrs · 23,204 cycles

STA 1417, STRINGER 30, LT TO 31, LT NEEDS EVALUATED FOR COMPLIANCE TO SRM. UPON REPAIR REMOVAL A DENT WAS DISCOVERED EXCEEDING SRM LIMITS. REA B652-59863-MR REV IR DATED 5/21/12 PROVIDED INSTRUCTION TO REMOVE THE DENT AND REPAIR IAW SRM 52-30-01, FIG 201.