N663GT

Part: TAMPER STRIP — MISSING (ELT) · airframe 115,190 hrs · 23,335 cycles

ELT -DO NOT REMOVE- TAPE WAS REMOVED. R &R ELT IAW AMM 25-63-03. OPS CHECKED GOOD.

Part: SEAL — BROKEN (ZONE 200) · airframe 114,361 hrs · 22,971 cycles

CAPTAIN EVAS TAMPER SEAL BROKEN(<P>INSTALLED NEW SEAL &AMP; NO FURTHER DEFECTS NOTED PER STC ST00892LA. DMI 237059 CLOSED</P>)

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

AFT CARGO BAY TORQUE BOX PANEL AT STATION 1280 RBL 29 FOUND WITH SURFACE CORROSION. WEB REMOVED AND REPLACED AS PER SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED.

Part: SKIN — CRACKED (ZONE 200) · airframe 114,051 hrs · 22,848 cycles

DURING HFEC OPEN HOLE INSPECTION ON LT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 10 O'CLOCK & 4 O'CLOCK POSITION VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CGO COMP'T - SHEAR CLIP AT STATION 742 S34L FOUND WITH SURFACE CORROSIONS AS MARKED. SHEAR CLIP (P/N: 140T2101Y21) AND SHEAR TIE (P/N: 140T2102U203) REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FUTHER DEFECTS NOTED.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CARGO COMPT WEB AT STATION 742 ABOVE S36L FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AS PER EN #3218-25. NO FURTHER DEFECTS NOTED.

Part: SKIN — CRACKED (ZONE 200) · airframe 114,051 hrs · 22,848 cycles

DURING HFEC OPEN HOLE INSPECTION ON RH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER. FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 1 O'CLOCK POSITON VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTS NOTED.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

AFT CARGO BAY TORQUE BOX PANEL BETWEEN STATION 1262 AND STATION 1285 RBL6 TO RBL 10 FOUND WITH SURFACE CORROSION. WEB REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CARGO BAY- SHEAR CLIP AT STATION 742 BETWEEN S37R AND S38R FOUND WITH SURFACE CORROSION. NEW SHEAR CLIP (P/N:140T2102U252) INSTALLED AS PER SRM 51-40-02 REV52. NO FURTHER DEFECTS NOTED.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CARGO COMPT WEB AT STATION 742 ABOVE S35L AND S36L FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AS PER EN #3218-25. NO FURTHER DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CARGO BAY SHEAR CLIP AT STATION 742 BETWEEN S35L AND S36L FOUND WITH SURFACE CORROSION. NEW SHEAR CLIP (P/N:140T2101Y21) AND SHEAR TIE (P/N:140T2102U243) INSTALLED AS PER SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,051 hrs · 22,848 cycles

FWD CGO COMP - SHEAR CLIP AT STATION 742 S37L FOUND WITH SURFACE CORROSIONS AS MARKED. SHEAR CLIP REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED.

Part: FUEL FILTER — WARNING MESSAGE (RT ENGINE) · airframe 113,521 hrs · 22,692 cycles

RIGHT ENGINE FUEL FILTER EICAS MESSAGE.(<P>REMOVED AND REPLACED RIGHT ENGINE FUEL FILTER AND THEN RIGHT ENGINE RUN CHECKED OK WITH NO LEAKEAGE FOUND, NO FAULT MESSAGE FOUND PER AMM 73-11-03/401.</P>)

Part: ADC — FAULTED (ZONE 200) · airframe 112,590 hrs · 22,519 cycles

AT 40,000' IN LEVEL FLIGHT, IAS DISAGREE MSG ON EICAS. CAPT'S AIRSPEED IND MAINTAINED 0.807M WHILE FO'S VARIED BY AS MUCH AS 0.03M &AMP; 12 KIAS. STBY A/S IND WAS CONCURRENT. FO'S A/S IND &AMP; CA'S A/S DETERMINED AS UNRELIABLE. ASSOC AIL LOCKOUT &AMP; RUDDER RATIO MSG ALSO PRESENT.(<P>REMOVED &AMP; REPLACED WITH NEW LH ADC THEN FUNCTIONAL TEST OF BOTH ADC PASSED IAW B767 AMM 34-12-01/401. NOTIFIED TO MCC. REF AIPC 34-12-01-02.</P>)

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 112,423 hrs · 22,489 cycles

CABIN ALT AUTO 2 EICAS MSG, CHANGE IN PRESSURIZATION, BRIEFLY DONNED OXYGEN MASKS(<P>TRANSFER TO DMI 215993 PER MEL 21-31-01A CAT C DUE DATE 13SEP24 REMOVED AND REPLACED CABIN PRESSURE CONTROLLER #2 IAW AMM 21-31-02 BITE CHECK PASSED THIS CLEARS MDDR 215993 ALL PLACARDS REMOVED PART REF IPC 21-31-02-0

Part: VALVE — LEAKING (AUTOBRAKE) · airframe 111,044 hrs · 22,075 cycles

MLG, LH MLG WHEEL WELL, VALVE MODULE SHUTTLE AUTOBRAKE WITH LEAK(<P>PART WAS REPLACED PER AMM 32-42-10-404-015. OPS CHK GOOD.</P>)

Part: SKIN — CORRODED (LT WINGLET) · corrosion level 2 · airframe 111,044 hrs · 22,075 cycles

LH WINGLET WEB SKIN (STA ZERO) CORROSION EVIDENCE(<P>LH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0107-07B &AMP; CMA-TLS 24-0107-12B. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (RT WINGLET) · corrosion level 2 · airframe 111,044 hrs · 22,075 cycles

RH WINGLET WEB SKIN (STA ZERO) EVIDENCE OF CORROSION(<P>RH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0105-03B. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DAMAGED (RT NR 7 SPOILER) · airframe 111,044 hrs · 22,075 cycles

RH WING SPOILER NO 7 HOLE (7 IN FROM LH EDGE & 5 IN FROM T/E)(<P>RH WING SPOILER #7 (AT 7" FROM INBD &AMP; 5" FROM T/E) LOWER SKIN WAS REPAIRED PER SRM 57-70-01-2R-1 &AMP; SRM 51-70-17-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 111,044 hrs · 22,075 cycles

RH WING INSPAR LOWER SURFACE WS 720.2 & STRINGER L-9 EVIDENCE OF CORROSION(<P>RH WING INSPAR LOWER SURFACE AT WS 720.2 &AMP; STRINGER L-9 WAS REPAIRED PER CMA-TLS 24-0108-01C * CMA-TLS 24-0108. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (RT IWNG TE FLAP) · airframe 111,044 hrs · 22,075 cycles

RH WING OUTBOARD FLAP LOWER SKIN EXISTING REPAIR WITH DELAMINATION (23 IN FROM L/E & 48 IN FROM LH EDGE)(<P>RH WING OUTBOARD FLAP LOWER SKIN PANEL WAS REPAIRED PER SRM 57-53-01-2R-1 &AMP; SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.</P>)

Part: IDG — UNKNOWN (UNKNOWN) · airframe 110,885 hrs · 22,017 cycles

TWO LOWSPEED RTO'S PERFORMED DUE TO L GEN OFF, L/R UTILITY BUS OFF SHORTLY AFTER APPLYING T/O POWER(<P>TRANSFER TO DMI 198358 PER MEL 24-00-01-01 CAT B DUE 06DEC2023. MX ACTIONS COMPLIED WITH VIA DISCONNECTION. PLACARDS INSTALLED. DISPATCH NOTIFIED. PERFORMED HIGH ENERGY STOP INSPECTION PER B767 AMM 05-51-14. NO DEFECTS NOTED. LP 1712717 M5: R/R LH ENG IDG IAW AMM 24-11-01. LEAK &AMP; OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MCC NOTIFIED. THIS CLEARS DMI 198358. PLACARDS REMOVED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,499 hrs · 21,884 cycles

L1 ENTRY DOOR WILL NTO CLOSE DUE TO EMERGENCY ESCAPE ROPE FALLING OUT OF CONTAINMENT POUCH(<P>STOWED EMERGENCY ROPE IAW AMM 25-61-04-402-010-001. L1 DOOR OPS CHECK NORMAL.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,139 hrs · 21,746 cycles

FLIGHT CONTROL FLUTTER ON LANDING(<P>PER ATLAS SAFETY DATA RETRIEVED INDICATED NO FLIGHT CONT ISSUES ON LANDING OR FLAIR. ACCOMPLISHED FLIGHT CONT/AILERON OPS TEST IAW AMM 27-11-00-215. NO DEFECTS NOTED.&NBSP;</P>)

Part: CONTROL ROD — UNKNOWN (UNKNOWN) · airframe 109,729 hrs · 21,614 cycles

UPON TAKEOFF, LE SLAT DISAGREE MESSAGE APPEARED ON EICAS. FOLLOWED QRH PROCEDURES. FLAPS WILL NOT MOVE TO UP POSITION. DIVERSION BACK TO SCK.(<P>REMOVED AND REPLACED #6 SLAT OB SLAT CONTROL ROD REF AMM 27-81-04-434-036 AND AMM 27-81-00-825-437. OPS CHECK SATISFACTORY AT THIS TIME. PERFORMED BITE OF FSEU, NO CURRENT FAULTS FOUND REF AMM 27-51-00.</P>)

Part: AILERON — CRACKED · airframe 109,022 hrs · 21,382 cycles

LH O/B AILERON I/B TRAILING EDGE NEAR FUEL DUMP TUBE REQUIRES EVALUATION FOR POSSIBLE CRACK (REPAIRED AILERON IAW B767-300 SRM BCG D634T210 REV121, 51-70-17-0G-0)

Part: EXTINGUISHER — LEAKING · airframe 108,882 hrs

FIRE BANE LIFE KIT FIRE EXTINGUISHER AGENT FOUND LEAKING. R & R FIREBANE LIFE KIT EXTINGUISHER IN OVERHEAD BIN IAW AMM 25-60-01. MCC NOTIFIED, PLACARDS REMOVED. NEW PART FILLED IN, OLD PART PREVIOUSLY REMOVED. MB 1757Z</P>)

Part: WARNING MESSAGE — ILLUMINATED (SHUTOFF VALVE) · airframe 108,844 hrs · 21,326 cycles

DURING CLIMBOUT, EICAS MSG DISPLAYED DURING HIGH POWER SETTING. RAN QRH CHECKLIST. L ENG HPSOV. TRANSFER TO MDDR 177720 IAW MEL 36-11-02-02 CAT C.

Part: NONE — NONE · airframe 108,469 hrs · 21,229 cycles

AT CRUISE PRIOR TO ETOPS ENTRY: RECEIVED "FUEL CONFIG" EICAS MSG. FUEL SUSEPTED. TOTALIZER &AMP; CALCULATED FUEL WERE 1500 LBS DEFFERENCE &AMP; INCREASING. FUEL QUANTITY INDICATING A 2,300 LBS SPLIT &AMP; INCREASING. COMPLIED WITH QRH, 1 ENG SHUT DOWN MANDAY RETURN TO HNL. L TANK INDICATED 2300 LBS LOWER THAN RIGHT &AMP; INCREASING TO MAX KNOWN 2600 LBS SPLIT.(<P>REMOVED AND REPLACED L/H FUEL TRANSFER &AMP; SHUTOFF VALVE PER B767 AMM 28-22-01-004-001 AND 28-22-01-404-011. OPERATIONAL CHECK GOOD IAW B-767 AMM 28-22-01-404-011. NO FUEL MIGRATION FOUND</P>)

Part: VALVE — LEAKING · airframe 107,945 hrs · 21,076 cycles

LH WING, REAR SPAR RIB 2 AT FUEL SHUT-OFF VALVE APU WITH EVIDENCE OF LEAK FUEL(<P>LH WING REAR SPAR RIB 2 AT FUEL SHUT OFF VALVE APU WAS REPLACED IAW AMM 28-25-02-404-008 REV 136 DATE 22 APR 2022</P>)

Part: ELT — BROKEN · airframe 107,945 hrs · 21,076 cycles

CONTROL CABIN, RH SIDE, LATERAL WALL OF LAVATORY, ELT WITH BROKEN SEAL(<P>EMERGENCY LOCATOR TRANSMITTER WAS REPLACED IAW AMM 25-63-03-000-802 &AMP; 25-63-03-400-802 REV 136</P>)

Part: PANEL — BURNED · airframe 107,945 hrs · 21,076 cycles

LH FUSELAGE AFT STATIC PORT THREE BURN MARKS NEAR LH STATIC PORT(<P>BURN MARKS WERE REPAIRED BY BLENDING OPERATIONS AND APPROVED BY BOEING IAW TRE6753549 DATE JUL 22, 2022</P>)

Part: DOOR — DENTED · airframe 107,945 hrs · 21,076 cycles

DENT WITH PREVIOUS REWORK AND ELONGATED HOLE AT STA 654+85 AND BEAM #3 OF LH MID ENTRY DOOR - OUTER SKIN(<P>DENT, PREVIOUS REWORK AND ELONGATED FASTENER HOLE WERE REPAIRED IAW TRE6752035</P>)

Part: PANEL — DELAMINATED · airframe 107,945 hrs · 21,076 cycles

ENGINE 1, ACOUSTIC SHROUD WITH SEVERAL DENTS BETWEEN 4 AND 7 HRS(<P>INLET COWL ACOUSTIC PANEL DENTS WERE REPAIR IAW EO 1971A286</P>)

Part: HOSE CONNECTOR — LEAKING · airframe 107,945 hrs · 21,076 cycles

NLG HYDRAULIC ACTUATOR, HOSE ASSY RH WITH SWEVEL LEAK(<P>NLG HYDRAULIC ACTUATOR, HOSE ASSY RH (P/N LPS14-49C8S) WAS REPLACED IAW AMM 32-34-01-004-027 &AMP; 32-34-01-404-010 REV 136</P>)

Part: PANEL — DENTED · airframe 107,945 hrs · 21,076 cycles

RH WING, BOTH OUTBOARD AILERON ACTUATORS (PCA) WITH EVIDENCE OF HYDRAULIC LEAK(<P>HYDRAULIC SYSTEM EXTERNAL LEAKAGE CHECK WERE PERFORMED. NO LEAKING EVIDENCE FOUND IAW AMM 29-11-00-796-053 REV 136</P>)

Part: SKIN PANEL — BURNED · airframe 107,945 hrs · 21,076 cycles

LH FUSELAGE AFT STATIC PORT THREE BURN MARKS(<P>BURN MARKS WERE REPAIR BY BLENDING OPERATIONS IAW TRE6753549 REV 0</P>)

Part: APU — LEAKING · airframe 107,945 hrs · 21,076 cycles

EVIDENCE OF FUEL LEAK AROUND ELECTRICAL WIRING CTR AUX FUEL QTY (M1934) LOCATED BETWEEN WBL 121 AND WBL 97.9566 AT REAR SPAR OF LH WING(<P>JAM NUT WAS TIGHTENED AND SEALANT WAS APPLIED AND CHEKED FOR LEAKS. TEST SATISFACTORY IAW AMM 28-41-04-404-028-002</P>)

Part: RADOME — DELAMINATED · airframe 107,945 hrs · 21,076 cycles

RADOME OUTER SKIN, HONEYCOMB AREA WITH IMPACT(<P>RADOME WAS REPLACED (NEW RADOME P/N 284T0052-39 S/N 000673) IAW AMM 53-12-01-A02-054</P>)

Part: BLEED AIR SYS — NOT SEATED · airframe 107,729 hrs · 21,008 cycles

L ENG BLEED OFF RTB KONT DUE TO PRESSUERIZATION/BLEED ISSUE. PERF AIR SUPPLY BITE PER FIM 36-20 FT 804.BITE FAULTED TEST FAILED WITH LIGHT TEST AND FAULTED MULTIPLE FAULTS ON BOTH L&R ENG. R&R SUPPLY BOX PER AMM 36-23-01. UPON FUTHER INSPECTION FOUND L ENG BLEED CARD NOT SEATED CORRECTLY R&R BLD CARD M859. PERF ENG IDLE RUN PER AMM 72-00-00 NO FAULTS FOUND NOTED L ENG BLD NORMAL.(CONT)LOG PG 1406455 R&RP; L ENG BLD CARD PER AMM 36-11-12. NO FAULTS NOTED. SYSTEM OPERATING NORMAL</P>)

Part: NONE — NONE

L ENG FUEL FILTER STATUS MSG(<P>INSPECTED FUEL FILTER ELEMENT IAW AMM 73-11-02-216-001-H00, NO CONTAMINATION FOUND. INSTALLED NEW FILTER ELEMENT IAW AMM 73-11-02-404-008-H00, RAN ENG IAW AMM 71-00-00-995-229-H03, NO LEAKS NOTED AND NO MSG ON EICAS DURING RUN.</P>)

Part: NONE — NONE · airframe 106,338 hrs · 20,640 cycles

FWD E&AMP;E COMPT CREW OXYGEN NEED SERVICE TO FULL(<P>REMOVED, SERVICED &AMP; REINSTALLED CREW OXYGEN CYLINDER AS PER&NBSP; B767-300 AMM&NBSP; 12-15-08</P> / <P>AMM&NBSP; 35-00-00-012-005,&NBSP; &NBSP;AMM&NBSP; 35-11-00-206&NBSP; &NBSP;AND&NBSP; &NBSP;AC&NBSP; 43.13-1B&NBSP; &NBSP;PAR&NBSP; &NBSP;9-46&NBSP; &NBSP;THRU&NBSP; &NBSP;9-51&NBSP; &NBSP;&AMP;&NBSP; NO LEAKS&NBSP; NOTED&NBSP; AT</P> / <P>THIS TIME. S/N&NBSP; &NBSP;OF THE&NBSP; CYLINDER&NBSP; SERVICED&NBSP; &NBSP; N840236.</P>)

Part: NONE — NONE · airframe 106,368 hrs · 20,640 cycles

#2 ENG O/B FAN COWL IS DELAMINATED(<P>ACCOMPLISHED&NBSP; HOT&NBSP; BONDED&NBSP; PERMANENT&NBSP; REPAIR&NBSP; ON&NBSP; #2&NBSP; ENG&NBSP; O/B&NBSP; FAN&NBSP; COWL&NBSP; PER&NBSP; 54-22-00-0G-0</P> / <P>54-21-01-0I-1,&NBSP; &NBSP;54-21-01-01A-1;&NBSP; 54-21-01-2R-1&NBSP; &NBSP; &NBSP;REPAIR 1</P> / <P>51-70-04-0G-0,&NBSP; &NBSP; &NBSP;WORK&NBSP; ACCOMPLISHED&NBSP; PER&NBSP; AVENIR&NBSP; AVIATION&NBSP; FAA #&NBSP; 8AVR479B&NBSP; &NBSP;FEAM&NBSP; RO #&NBSP; 5002790</P> / <P>AND&NBSP; &NBSP;AVENIR&NBSP; &NBSP;WO&NBSP; #W16039&NBSP; &NBSP; &NBSP; &NBSP;8130&NBSP; ATTACHED</P>)

Part: NONE — NONE · 20,617 cycles

"WX SYS" STATUS MSG AFTER TAKEOFF (REMAINED ENTIRE FLT)(<P>PERFORMED FIM TASK 34-43 TASK 801. FAULT CLEARED. WEATHER RADAR SYSTEM OPS CHECKS GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS)

ON TAXI IN THE "WXR SYS" STATUS MESSAGE DISPLAYED(<P>C/W WEATHER RADAR SYSTEM OPERATIONAL TEST IAW AMM 34-43-00-715-026-002. OPS CHECK GOOD.</P>)

Part: CIRCUIT CARD — FAULTED (BLEED OVERHEAT)

REPEATED, R BLD DUCT LEAK ON GROUND W/APU RUNNING, NO ENGINES RUNNING.(<P>REPLACED WHEEL WELL BLEED OVHT CARD IAW B767-300 AMM 36-21-00. RAN PACKS 30 + MIN WITH NO RECURRENT FAULTS.</P>)

Part: ENGINE — VIBRATION (NR 2)

NO. 2 ENGINE FAN VIBRATION LEVEL INCREASES BETWEEN FL200 TO FL340 BETWEEN MAT VALVES OF 3.0 TO 4.0. ALSO DURING INTERMEDIATE CLIMB ABOVE FL340.(<P>ACCOMPLISHED VIBE SURVEY IAW 767 AMM 71-00-00 TEST #6. AT MPA VIBES WERE THE HIGHEST&NBSP; #1 ENG VIBE WAS FAN AT 1.2 AND #2 ENG VIBE WAS FAN AT 2.3. WITHIN LIMITS IAW 767 AMM 71-00-00. OK FOR SERVICE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU OIL) · 20,515 cycles

APU FAULT LIGHT DURING FIRST START ATTEMPT. APU OIL STATUS INDICATION "ADD"(<P>C/W FIM - 49-11-43958. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: FILTER — FAILED (RT FUEL)

R ENG FUEL FILT EICAS MESSAGE DURING CLIMB OUT INTERMITTENT 3 TIMES. ACCOMPLISHED QRH.(<P>REMOVED &AMP; REPLACED R ENG FUEL FILTER IAW AMM 73-11-02. ALSO COMPLETED FUEL FILTER ELEMENT TEST PER AMM 73-11-02-724. ALL CHECK GOOD. NO LEAKS NOTED. OPS CHECK GOOD.</P>)

Part: HYDRAULIC SYSTEM — LEAKING · airframe 105,776 hrs · 20,507 cycles

#2 ENG. HAS EVIDENCE OF HYD. LEAK AT FWD AREA ( COMP ) FROM 9 O'CLOCK TO 3 O'CLOCK . CLEANED RT THRUST REVERSER OPEN/CLOSE ACTUATORS CLEANED & RETORQUED NR 2 ENG LT & RT T/R OPEN / CLOSE ACTUATOR LINE IAW AMM 12-25-00 & AMM 78-31-06. LEAK CK PEFORMED PER AMM 29-11-00, NO LEAKS.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 105,776 hrs · 20,507 cycles

ENG 1 PRVC LOC E FOUND TO BE LEAKING. ENG #1 PNEUMATIC SEAL& REPLACED AND TORQUED IAW 20-11-00. LEAK CHECK GOOD.

Part: IDG — INOPERATIVE (LT GENERATOR) · airframe 105,776 hrs · 20,507 cycles

LH ENGINE IDG INOP(<P>REMOVED AND REPLACED&NBSP; # 1 ENG&NBSP; IDG&NBSP; IAW AMM 24-11-01.</P> / <P>PENDING FOR OPS &AMP; LEAK CHECK .</P> / <P>PERFORMED OPS CHK PER AMM 24-11-.</P> / <P>OPS CHK GOOD. NO LEAKS.</P>)

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 105,776 hrs · 20,507 cycles

ENG 1 PRVC LOC K FOUND TO BE LEAKING. REMOVED AND REPLACED DEFECTIVE PACKING IAW MM 36-11-18-404-018-001. STEP 10. LEAK CHECK GOOD.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 105,776 hrs · 20,507 cycles

ENG 2 PRVC LOC K FOUND TO BE LEAKING(<P>REMOVED AND REPLACED PACKING AT LOCATION "K" PER EO 1936A088 &AMP; AMM 36-11-18</P> / <P>NO&NBSP; LEAKS</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYSTEM)

WXR SYS STATUS MESSAGE(<P>PERFORMED OPS TEST PER AMM 34-43-00. FAULT CLEARED. OPS TEST PASS. AC IS OK TO CONTINUE.</P>)

Part: FIRE LOOP — CONTAMINATED (LT ENGINE)

L ENG FIRE LP 2 EICAS STATUS MESSAGE AFTER TAKEOFF(<P>FWD TO MDDR 151582 IAW MEL 26-11-01-01. CAT C. DUE DATE 19AUG21.</P> / <P>LP 1247995 ITEM 10: T/S PER FIM 26-11-F/T 805 .CLEANED UP CONTAMINATED LH ENG FIRE LOOP DETECTOR SYS, OPS CKS PER AMM 26-11-00 REV 132. MDDR 151582 CLEARED. PLAC REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP)

INTERMITTENT L FIRE LOOP STATUS MESSAGE(<P>COULD NOT DUPLICATE. PERFORMED FIM AND OPS CHECKED GOOD IAW MM 26-11-00.</P>)

Part: IDG — FAULTED (NR 1) · 20,507 cycles

L GEN OFF EICAS CAUTION MESSAGE, FAILURE WAS ASSOCIATED WITH A LARGE JOLT, POSSIBLE COMPRESSOR STALL @7 MIN INTO FLIGHT EVENT(<P>LP 1247984, ITEM M4: ACCOMPLISHED BORESCOPE INSPECTION OF HPC STAGES I,6,7,12 &AMP;13 AND HPT STAGES 1 AND 2 AS PER ATLAS P.P. ENGINEERING REQUEST FOR POSSIBLE COMPRESSOR STALL ON ENGINE, AND LPC STAGES 2 AND 5. ALL NOTED WITHING SERVICEABLE LIMITS REF B767-300 AMM 72-00-00-706-300-P00. EVIDENCE OF BIRD TRIKE INGESTION ON LPC 2,5 AND HPC 1. NO DAMAGE NOTED.</P> / <P>TRANSFERRED TO MDDR 151509 PER MEL 24-00-01-01, CAT B.</P> / <P>LP 1247995 ITEM 11: REMOVED AND REPLACED #1 ENGINE IDG PER AMM 24-11-01. PERFORMED OPS CHK, OPS CKD GOOD, NO LEAKS NOTED.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT FIRE LOOP)

AFTER TAKEOFF STATUS MESSAGE "L ENG FIRE LOOP 2" STATUS MESSAGE CLEARED ON ITS OWN AFTER 15MINUTES(<P>NO MESSAGE UPON ARRIVAL. BITE BITE CHK AFDLTS SYSTEM. NO FAULTS NOTED. BITE TESTED PER AMM TASK 26-10-20-716-019. OK TO CONTINUE.</P>)

Part: OXYGEN MASK — BROKEN (PORTABLE OXYGEN) · airframe 105,743 hrs

PORTABLE OXYGEN BOTTLE AT L1 DOOR MASK BROKEN(<P>TRANSFERRED TO MDDR 151338 IAW MEL 35-31-01, CAT D.&NBSP;</P> / <P>LP<SPAN>1342039: </SPAN><SPAN>REMOVED AND REPLACED MASK IAW AMM 35-31-01 CKS GD THIS CLEARS MDDR 151338, PLACARD REMOVED</SPAN></P>)

Part: WARNING HORN — FALSE ACTIVATION (APU) · 20,486 cycles

AFTER LANDING EICAS MSG "APU FAULT" AFTER 1ST START ATTEMPT. 2ND ATTEMPT SUCCESSFUL. STATUS PAGE SHOWED "ADD" OIL QUANT FOR APU, BUT LATER SHOWED "FULL". PERFORMED APU BITE PROCEDURES IAW FIM 49-11-00-815-987-004. NO FAULTS NOTED. CHECKED APU OIL QTY IAW AMM 12-13-04-200-801. OIL LEVEL FULL.& A/C OK TO CONTINUE.

Part: FIRE LOOP — NOT REPORTED (LT ENGINE) · airframe 105,540 hrs · 20,455 cycles

L ENG FIRE LOOP 2(<P>TRANSFER TO MDDR #150042 IAW MEL 26-11-01-01, CAT C, EXP 23JUL21. DP @ 1108Z.</P> / <P>14JUL21 - LP 1310333 - ITEM# 1 - MEM - REMOVED AND REPLACED UPPER AFT FIRE LOOP IAW AMM 26-11-02. THIS CLEARS MDDR 150042.</P>)

Part: IDG — FAULTED (LT GENERATOR) · airframe 105,505 hrs · 20,448 cycles

ON LEFT ENG START, LEFT GEN AUTO DISCONNECT EICAS MSG "L GEN OFF" &AMP; L GEN DRIVE".(<P>REMOVED &AMP; REPLACED #1 ENG IDG IAW B767 AMM 24-11-01. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME.</P>)

Part: TRANSMITTER — MALFUNCTIONED (APU OIL)

APU OIL QTY INOPERATIVE. C/W W/O 85469, REMOVED AND REPLACED APU OIL QTY TRANSMITTER IAW B767-300 AMM 49-94-04. OPS CHECK GOOD. NO LEAKS NOTED.

Part: INDICATOR — INOPERATIVE (TRIM VALVE) · airframe 105,454 hrs · 20,434 cycles

TRIM AIR VALVE POSITION INDICATOR INOP ( TRIM AIR VALVE POSITION INDICATOR )(<P>FWD TO MEL 21-64-01, MDDR #149493, CAT C, DUE DATE 11JUL21.</P> / <P>LP 1463337: REMOVED AND REPLACED TRIM AIR VALVE POSITION INDICATOR IAW AMM 21-64-01. OPS CHECK GOOD. THIS CLOSES MDDR 149493. PLAC REMOVED.</P>)

Part: APU — FAULTED · airframe 105,412 hrs · 20,423 cycles

APU RELIABILITY COLD SOAK START 1ST ATTEMPT-APU FULLY STARTED THEN SHUT DOWN AFTER 5 MINUTES. FAULTED DURING 2ND ATTEMPT. 3 ATTEMPT 850-45 DEG, RAN FOR 15 MINUTES THEN FAULTED.(<P>FOUND ECU FAULTING ITSELF. PART TO BE REPLACED 25JUN21 IF RECEIVED. APU TRANSFERRED TO MDDR 149154 IAW MEL 49-11-01A. CAT C. DUE DATE 04JUL21. MCC NOTIFIED. ACL @ 21:28Z.</P> / <P>LP 1463341: REMOVED AND REPLACED APU IAW W/O 83082. APU OPS CHECK GOOD IAW AMM 49-11-00. THIS CLEARS DMI 149154.

Part: ACTUATOR — FAULTED (APU) · airframe 105,420 hrs

APU FAIL(<P>TRANSFERRED TO MEL 49-11-01A, CAT C, EXP DATE 13JUL21, MDDR 149054.</P> / <P>LOG 1310365 ITEM #2: REMOVED AND REPLACED APU IGV ACTUATOR IAW B767-300 AMM 49-52-02. OPS CHECK GOOD. APU SPOOLS UP FASTER. MDDR 149054 REMAINS OPEN.</P> / <P>LOG 1310365 ITEM #3&NBSP; REMOVED AND REPLACED APU OIL QTY TRANSDUCER (OFF PART: PN&NBSP;<SPAN>3886167-4</SPAN><SPAN>, SN&NBSP;</SPAN><SPAN>0662</SPAN><SPAN>) IAW B767-300 AMM 49-94-04. OPS CHECK GOOD, LEAK CHECK GOOD. THIS CLEARS DMI #149054, PLACARD REMOVED, MCC NOTIFIED.</SPAN></P>)

Part: MONITOR — MALFUNCTIONED (FAN VIBRATION) · 20,419 cycles

ON CLIMB OUT OF SJU #2 ENG FAN VIB CLIMB TO 4.3 DECREASED AT LEVEL OFF CRUISE ALT NO VIBS FELT(<P>PER POWERPLANT ENGINEER, READINGS FROM ENG BIB MONITOR SEEM TO BE ERRONEOUS AND INCONSISTANT. UNIT TO BE REPLACED ON LONGER GROUND TIME PER ACTION PLAN. TRANSFERRED #2 ENG VIB MONITOR UNIT TO MDDR # 148709 IAW MEL 77-31-01, CAT C, DUE 27 JUN21.</P> / <P>18JUN21 - LP 1341791 - M2 - MEM - PERFORMED OPS CHECK VIBRATION MONITOR UNIT IAW B767 AMM 77-31-05. OPS CHECK GOOD. THIS CLEARS MDDR 148709, PLAC REMOVED. MCC NOTIFIED.</P>)

Part: BATTERY — FAILED (APU) · airframe 105,397 hrs · 20,409 cycles

APU FAILED TO START AFTER TWO ATTEMPTS, REPEAT WRITE UPS(<P>TRANSFERRED TO MDDR 148462 IAW MEL 49-11-01A, CAT C, DUE DATE 22JUN21.</P> / <P>17JUN21 - 1341786 - ITEM# 2 - MEM - REMOVED AND REPLACED APU BATTERY IAW B767-300 AMM 24-31-04. OPS TEST GOOD. 6X GOOD STARTS. THIS CLEARS MDDR 148462. MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 105,350 hrs · 20,407 cycles

LEFT ENGINE FIRE LOOP ONE STATUS MESSAGE(<P>PERFORMED FIRE TEST IAW 26-11-00-75, FAULT CLEARED.</P>)

Part: FIRE LOOP — INTERMITTENT (LEFT) · airframe 105,304 hrs · 20,395 cycles

LEFT ENGINE LOOP 1 STATUS INTERMITTENT(<P>TRANSFERRED TO MDDR 148251 IAW MEL 26-11-01-01, CAT C, DUE 18DEC. PLACARDS INSTALLED.</P><P>LP&NBSP;<SPAN>1277117:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED FWD AND AFT #1 ENGINE FIRE LOOP IAW 767 AMM 26-11-02-401. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 148251. MCC NOTIFIED.</SPAN></P>)

Part: LINE — INOPERATIVE (LT A/C PACK) · airframe 105,312 hrs · 20,397 cycles

LH PACK INOP(<P>TRANSFERRED LH PACK TO MDDR 148075 IAW MEL 21-51-01-01, CAT C, DUE 15JUN21. MX PROCEDURES C/W. PLACARDS INSTALLED.</P><P>LP&NBSP;1277104 M6: REMOVED AND REPLACED HOT AIR SUPPLY LINE CONNECTED TO CONDENSER IAW AMM 20-10-10, OPS CHECKS GOOD IAW AMM 21-51-50. NO LEAKS NOTED @ THIS TIME. THIS CLEARS MDDR 148075. MCC NOTIFIED CW @ 2215Z</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 105,293 hrs · 20,392 cycles

AFT EQP EXH FAN 2 STATUS MESSAGE(<P>FAULT CLEARED, REF FIM 21-58-00 FAULT TREE A 02</P>)

Part: ECU — FAULTED (ECU) · airframe 105,312 hrs · 20,397 cycles

APU FAILED TO START(<P>TRANSFERRED TO MDDR# 148078 IAW MEL 49-11-01A, CAT C, DUE 15JUN21. REMOVED AND REPLACED APU FCU IAW AMM 49-31-01-644-045. OPS CHECKED GOOD. NO LEAKS NOTED.

Part: MODULATING VALVE — FAILED (NR 2 ENGINE) · airframe 105,258 hrs · 20,382 cycles

OPS CHECK OF #2 ENG FAN MODULATING VLV, CHECKED BAD.(<P><SPAN>TRANSFERRED TO MDDR # 147892, CAT C. DUE 11JUN21 IAW MEL 36-12-02-01. MCC NOTIFIED. PLACARDS INSTALLED, LEAK CHECK GOOD. JL AT 1648Z.</SPAN></P><P>REMOVED AND REPLACED RH FAN AIR MODULATING VALVE IAW B767 AMM REF 36-11-16. OPS CHECKED GOOD. THIS CLEARS MDDR 147892, MCC NOTIFIED. TS @ 01:17Z</P>)

Part: MOTOR — FAILED (APU STARTER) · airframe 105,301 hrs · 20,385 cycles

APU FAILED TO START(<P>TRANSFERRED TO DMI 147803 IAW MEL 49-11-01B. COMPLIED WITH MAINT. PROCEDURES.</P><P>05JUN21 - LP 1281673: REMOVED AND REPLACED APU STARTER ASSEMBLY IAW B767-300 AMM 49-41-01. OPS CHECKED GOOD. THIS CLEARS MDDR 147803. MCC NOTIFIED.

Part: STATUS MESSAGE — FALSE INDICATION (APU OIL SYSTEM) · airframe 105,193 hrs · 20,373 cycles

APU OIL QTY STATUS MESSAGE.(<P>PERFORMED B767-200/300 FIM TASK 49-11 FAULT TREE A02, SERVICED APU WITH 2 QTS. SYSTEM SATISFACTORY. APU ECU BITE OK, SELF TEST OK.</P>)

Part: METERING UNIT — FAULTED (OXYGEN SYSTEM) · airframe 105,120 hrs · 20,362 cycles

CREW O2 READS 40 PSI ON EICAS. VERIFIED BOTH O2 BOTTLES ARE OPENED AND PRESSURE ON BOTTLES ARE AT 1600 PSI EACH.(<P>TRANSFERRED TO DMI # 147139 IAW MEL 35-11-02-01. CAT "B" DUE 21MAY21. PLACARDS INSTALLED. VERIFIED BOTH O2 ARE ON AND BOTH BOTTLE AVERAGE IS 1600 PSI. T/I: DL 0522Z.</P><P>19MAY21, AMS MX: LP 1464799, ITEM 1: REPLACED AVERAGING UNIT PER AMM 25-11-06. REVERSED MEL PROCEDURES, ALL INDICATION RETURNED. DMI 147139 CLOSED. MCC RG 14:35Z, DISP DP 1441Z</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 105,094 hrs · 20,358 cycles

INFLIGHT INTERMITTENT "MN CARGO LOOP 1" AND "MN CARGO LOOP 2" STATUS MESSAGES(<P>PERFORMED FIM TASK 26-14 FAULT TREE 809. OPS CHECKS GOOD, MAIN CARGO COMPARTMENT SMOKE DETECTION SYSTEM IS OK FOR SERVICE</P>)

Part: APU — MALFUNCTIONED · airframe 104,933 hrs · 20,336 cycles

APU FAILED PRIOR TO PUSH(<P>NO RELATED FAULTS ON EICAS, APU BITE SHOWS "REVERSE" FLOW FAULT. PERF APU BITE, NO FAULTS PERF. APU OPS CHECK IAW AMM 49-11-00 TEST OK. OK FOR SVC.</P>)

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 104,557 hrs · 20,290 cycles

R ENG STARTER EICAS ILLUMINATES AND EXTINGUISHES DURING R ENG START. NORMAL DUCT PRESSURE OBSERVED(<P>REMOVED AND REPLACED ENGINE (RH) START VALVE IAW AMM 80-11-02. DRY MOTOR CHECK GOOD PER AMM 71-00-00-712-168-H03.<BR /></P>)

Part: TRANSMITTER — MALFUNCTIONED (FUEL FLOW) · airframe 104,425 hrs · 20,274 cycles

39 MIN INTO FLIGHT FL410 FUEL FLOW READING LT 0.5 R7 3.8 CALCULATED FUEL READING (FUEL USED) LEFT 0.0 TOT 4.3 RIGHT 4.3 (REMOVED AND REPLACED LT ENG FUEL FLOW TRANSMITTER, NO LEAKS NOTED, OPS CHECK NORMAL IAW AMM 73-31-01. PERFORMED ENGINE RUN UP, OPS CHECK NORMAL IAW 71-00-00).

Part: SWITCH — INOPERATIVE (FUEL PUMP PRESS) · airframe 104,413 hrs · 20,271 cycles

RIGHT AFT FUEL PUMP LOW PRESSURE INDICATION INOPERATIVE. R & R RT AFT FUEL PUMP PRESSURE SWITCH REF AMM 28-42-01. OPERATIONAL CHECK AND LEAK CHECK GOOD.

Part: STARTER — INOPERATIVE (APU) · airframe 104,263 hrs · 20,252 cycles

APU FAULT ATTEMPTED 3 TRIES BUT NEVER STARTED. REMOVED AND REPLACED APU STARTER MOTOR ASSEMBLY, PER AMM 49-41-01. OPERATIONS CHECK CW AND APU START SUCCESFUL.

Part: FILTER — UNKNOWN (FUEL SYSTEM) · airframe 104,296 hrs · 20,256 cycles

LT FUEL FILTER EICAS MESSAGE. REMOVED AND REPLACED LT ENGINE FUEL FILTER ELEMENT, PER AMM 73-11-02. MESSAGE CLEARED. LEAK CHECK GOOD.

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 104,172 hrs · 20,240 cycles

WEATHER RADAR SYSTEM 1 INOPERABLE "WXR FAILED" MESSAGE. NO STATUS MESSAGE FOUND. PERFORMED WX RADAR AND TEST AND OPERATIONS CHECK, IAW AMM 34-43-00 AND FOUND ALL SATISFACTORY.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL PUMP) · airframe 104,165 hrs · 20,239 cycles

RIGHT CENTER FUEL PUMP EICAS AND PRESS LIGHT ILLUMINATED, PUMP ON AND 3000 LBS OF FUEL IN CENTER TANK. C/O OPERATIONS CHECK RIGHT CENTER FUEL PUMP, IAW AMM 28-31-00 AND FOUND SATISFACTORY.

Part: CONTROL VALVE — MALFUNCTIONED (APU BLEED SYS) · airframe 104,149 hrs · 20,237 cycles

APU DUCT PRESSURE SURGING 5 -15 PSI WITH PACKS RUNNING. AFTER TROUBLESHOOT AND RESET APU BLEED AIR AND CONTROL CB. DUCT PRESSURE NORMAL, PER MCC REQUEST APU PNEUMATICS DEFERRED TO MDDR 139986, CAT C, MCC TODD C LC 12:12Z, DDG 49-11-01-01. REPLACED APU SURGE CONTROL VALVE AND RUBBER DUCT, IAW AMM 49-53-01. OPERATIONS CHECK AND LEAK CHECK GOOD.

Part: RADAR — FAILED (WEATHER SYS) · airframe 103,975 hrs · 20,212 cycles

WX RADAR 1 AND 2 FAILURE IN FLIGHT. WX SYSTEM MESSAGE DISPLAYED. 18NOV20/1270889/ITEM M10/AMS. PERFORMED OPERATIONS CHECK OF LT AND RT WX SYSTEM, IAW AMM 34-43-09 AND FOUND WORKING SATIFACTORY.

Part: DRIVE ASSY — FAILED (WX RADAR ANTENNA) · airframe 103,959 hrs · 20,210 cycles

WX SYS 1 AND 2 FAIL IN FLIGHT. ITEM M13-FOUND ANTENNA DRIVE FAIL REPLACED WX ANTENNA DRIVE, IAW AMM 34-43-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 103,959 hrs · 20,210 cycles

RADAR SYSTEM 1 AND 2 FAILED IN FLIGHT, WXR SYSTEM STATUS MESSAGE DISPLAYED AND SYSTEM 1 AND 2 FAILED AT SAME TIME. PERFORMED WXR SYSTEM OPERATIONAL CHECK, PER 34-43-00. OPERATIONS NORMAL, NO FURTHER MESSAGE. NO DEFECTS NOTED.

Part: CIRCUIT CARD — MALFUNCTIONED (STALL WARNING) · airframe 103,935 hrs · 20,207 cycles

ADI FAILURE FLAG "SPD LIM". REMOVED AND REPLACED LEFT STALL WARNING M615 CARD, REF AMM 27-32-01. STALL WARN TEST PASSED.

Part: ELT — DAMAGED (CABIN) · airframe 103,893 hrs · 20,201 cycles

ON PREFLIGHT SURVIVAL ELT WATER SOLUBLE TAPE COVERED IN MASKING TAPE. WATER SOLUBLE TAPE BROKEN. PLACED ON DMI 137291, MEL 25-63-10-02A, CAT A, DUE ON 04FEB21 RS 0052Z 06NOV20. REMOVED AND REPLACED SURVIVAL ELT, IAW IAI SUPPLEMENT 25-63-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 103,812 hrs · 20,191 cycles

IN CRUISE FLT, ON HSI AMBER MESSAGE "WXR FAIL". PERFORMED ACC FIM TASK 34-43. FAULT TREE A05 TEST OK AFTER RESET C/B OVERHEAD PANEL F2 AND F23.

Part: COOLING DUCT — OUT OF POSITION (COCKPIT) · airframe 103,399 hrs · 20,113 cycles

EXCESSIVE COLD AIR BLOWING FROM LIFT RUDDER PEDDLE FO SIDE(<P>PER B767 IPC 21-58-31-01 COOLING DUCT IS AT THE CORRECT LOCATION. NO FAULTS NOTED.<BR /></P>)

Part: OXYGEN BOTTLE — DAMAGED (PORTABLE) · airframe 103,389 hrs · 20,110 cycles

ON WALK AROUND, THE O2 BOTTLE HAD BROKEN COVER FOR MASK ATTACH POINT. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01

Part: EADI — FAILED (CAPTAIN'S) · airframe 103,346 hrs · 20,094 cycles

CA SIDE EADI FAILURE IN FLIGHT FL 390. EFI SWITCH INEFFECTIVE REMOVED AND REPLACED CA EADI IAW AMM 34-22-03. OPS CHECK GOOD.

Part: EADI — FAILED (CAPTAIN'S) · airframe 103,236 hrs · 20,061 cycles

SHORTLY AFTER TAKE OFF, CA HSI AND ADI GO FULL BRIGHT WITH NO INPUT FROM CA FO HEARD CLICKING, & ENTIRE CREW SMELLED FUMES, BRIGHT RED SQUARE APPEARS ON CA HSI, THEN WENT BRIGHT ORANGE WITH APPEARANCE OF SPARK LOOKING DOT IN CENTER HSI FAILED, EFI SWITCH PUSHED, HSI CAME BACK ON THEN FAILED AGAIN ADI SURGED IN BRIGHTNESS THEN TURNED BLURRY. REMOVED AND REPLACED THE CAPTAIN`S EHSI IAW AMM 34-22-04. OPS CHECKED NORMAL.

Part: EADI — FAILED (CAPTAIN'S) · airframe 103,106 hrs · 20,043 cycles

CAPTAIN`S EADI AND EHSI BLANKED, FOLLOWED BY THE ODOR OF BURNING. ELECTRICAL EQUIPMENT, OXYGEN MASKS WERE ON AND EMERGENCY DECLARED. DISINFECTED AND RESTOWED THE OXYGEN MASKS IAW B767 AMM 35-11-51.

Part: IGNITER — DEFECTIVE (RT ENGINE) · airframe 102,953 hrs · 20,021 cycles

RT ENGINE FAILED TO START W/ SINGLE IGNITER. SECOND ATTEMPT IN BOTH SUCCESSFUL. R ENGINE BOTH IGNITER PLUGS IN POOR CONDITION, REPLACED BOTH PLUGS IAW AMM 74-21-02. TESTED SATISFACTORY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,961 hrs · 20,022 cycles

DURING CRUISE, FLT STATUS MSG WXR SYS AND LOWER EHSI SCREEN WXR ATI MSG FOR RADAR SYSTEM. CLEARED WXR MESSAGE AND PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM. REF AMM 34-43-00. OPERATIONAL TEST GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 102,830 hrs · 19,984 cycles

STATUS MSG WX SYS(<P>PERFORMED OPS TEST OF WXR SYS REF B767 AMM FIM TASK 34-43 F/T 805, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.</P>)

Part: VALVE — MALFUNCTIONED (COCKPIT TEMP) · airframe 102,761 hrs · 19,959 cycles

FLT DECK TEMP EICAS.(<P>TRANSFERRED TO MDDR 127529, IAW DDG 21-61-02-03 CAT "C".</P><P>LP 822320: REPLACED TRIM AIR VLV, CKS GOOD. CLOSED MDDR 127529 IAW AMM 21-61-07.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,752 hrs · 19,957 cycles

EICAS MSG: L PACK TEMP OCCURRED AT TOP OF CLIMB FL 410 TAT -26, SAT -54.(<P>PERFORMED FIM PROCEDURE 21-51 F/T 803. NO DEFECTS NOTED ON PACK TEMP CONTROLLER BITE TEST. EICAS MSG CLEARED.</P>)

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 102,748 hrs · 19,955 cycles

CAPTS MFO BLANKED TWICE WITH AN AUDIBLE POPPING SOUND &AMP; OZONE SMELL HSI CB @ E6 HAS POPPED AS WELL.(<P>SWAPPED LOWER EICAS DU WITH CAPT'S HSI DU, SYSTEM CK'S GOOD IAW MM CH 34-22-04. P/N 622-7999-003 S/N 1658 NOW IN CAPT'S EHSI POS. P/N 622-7999-003 S/N 3966 NOW IN LOWER EICAS POS.</P><P>LP 822314, ITEM M5: VERIFIED BURNT SMELL EMITTING FROM CAPT'S EHSI D.U., NO OTHER FUMES OR SMELL OF SMOKE NOTED IAW MM CH 05-51-56.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,752 hrs · 19,957 cycles

"L PACK TEMP" DISPLAYED INTERMITTENTLY IN FLIGHT(<P>PERFORMED FIM PROCEDURE 21-51 F/T 844. NO FAULTS FOUND ON PACK TEMP CONTROLLER BITE TEST. EICAS MSG CLEARED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,748 hrs · 19,955 cycles

"L PACK TEMP" DISPLAYED INTERMITTENTLY INFLIGHT.(<P>PERFORMED FIM PROCEDURE 23-51 F/T 844. NO FAULTS FOUND ON PACK TEMP CONTROLLER BITE TEST. EICAS MSG CLEARED.</P>)

Part: SWITCH — FAULTY (ANTI-ICE SYS) · airframe 102,673 hrs · 19,928 cycles

R ENGINE ANTI ICE EICAS, QRH PERFORMED.(<P>REMOVED AND REPLACED VALVE ANTI ICE #2 ENG IAW AMM 30-21-03. OPS TEST OK (OFF PART: PN&NBSP;<SPAN>2790583-108</SPAN><SPAN>, SN&NBSP;</SPAN><SPAN>3029F</SPAN><SPAN>).</SPAN></P><P>LP 822296 ITEM 5: REMOVED AND REPLACED #2 ENG INLET THERMAL ANTI ICE OVERHEAT SW IAW AMM 30-21-04. OPS TEST OK.</P>)

Part: CONTROL PANEL — FAULTY (ANIT-ICE SYSTEM) · airframe 102,614 hrs · 19,907 cycles

RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED AFTER DEACTIVATING SYSTEM.(<P>TRANSFERRED TO MDDR 125466 IAW DDG 30-21-02-01A, CAT "C", DUE 17MAR20.</P><P>LP 822266: REMOVED AND REPLACED&NBSP;RIGHT ENGINE ANTI-ICE CONTROL PANEL IAW AMM 30-11-01. OPS CHECK NORMAL. THIS CLEARS DMI 125466. PLACARD REMOVED.<BR /></P>)

Part: IGNITER — DEFECTIVE (LT ENGINE) · airframe 102,592 hrs · 19,902 cycles

LP 822383-1 - STATUS MSG - LH ENG IGNITER NR 2 - (SEE DISCREPANCY ITEM NR 02)&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; LP 822383-2 - INFO ONLY - LH ENGINE NO LIGHT OFF ON FIRST START ATTEMPT. PLACED ENG START SELECTOR IN BOTH. NORMAL START SECOND ATTEMPT.(<P>LP 822383-1 AND -2:&NBSP; REMOVED AND REPLACED LH ENG IGNITER PLUG NR 2 IAW AMM 74-21-02, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.</P><P>LP 822383-3: PER MCC REQUEST (DUE LH ENG IGNITION HISTORY), REMOVED AND REPLACED RELAY K1251 (OFF PART: PN BACR13C62A, NSN) IAW SWPM 20-81-00 AND WDM 74-31-11, RAN ENGINE IAW 71-00-00 IN SINGLE START TWICE. BOTH RUNS NORMAL. NO STATUS MSG, OPS CHECK GOOD.</P>)

Part: GAUGE — DAMAGED (O2 BOTTLE) · airframe 102,581 hrs · 19,900 cycles

CREW O2 APPROACHING MINIMUMS @ 1430 PSI.(<P>UPPER CREW O2 BOTTLE INDICATING GAUGE FOUND TO BE DAMAGED. REMOVED AND REPLACED UPPER CREW O2 BOTTLE IAW AMM 12-15-08-603-001 &AMP; GMM 3.25.3. LEAK CHECK GOOD. OPS NORMAL.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,610 hrs · 19,906 cycles

RH ENG ANTI-ICE VALVE LIGHT ILLUMINATED AFTER LANDING WHEN SHUTTING ANTI-ICE OFF.(<P>PERFORMED ENG RUN AND OPS CHECK OF RT ENG ANTI ICE VALVE IAW B767 AMM 71-00-00 AND AMM 30-21-03. OPS CHECK GOOD. NO FAULTS FOUND AT THIS TIME.&NBSP;</P>)

Part: CONTROL PANEL — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 102,572 hrs · 19,896 cycles

AFTER R ENG SHUTDOWN IN THE BLOCKS, THE RIGHT ENG ANTI-ICE VALVE FAILED TO CLOSE WITH THE SWITCH SELECTED OFF, VALVE LIGHT STAYED ILLUMINATED.(<P>REMOVED AND REPLACED WING AND ENG ANTI-ICE PANEL ASSY IAW B767 AMM 30-11-01.&NBSP;<BR /></P>)

Part: CONTROL PANEL — MALFUNCTIONED (LT ENGINE) · airframe 102,545 hrs · 19,888 cycles

NO LIGHT OFF LEFT ENGINE, START SELECTOR IN SINGLE. SUCCESSFUL START ON BOTH.(<P>TRANSFERRED TO MDDR #124988 IAW MEL 74-00-01B CAT C DUE DATE 04MAR20.</P><P>LP 822360 - M2:&NBSP;REMOVED AND REPLACED L ENG #2 IGNITION EXCITER IAW B767 AMM 74-11-01-004-001 (OFF PART: PN&NBSP;10-631045-3A, SN&NBSP;UNLCD872).</P><P>LP 822360 - M3:&NBSP;REMOVED AND REPLACED L ENG #2 IGNITION LEAD IAW B767 AMM 74-21-01-404-028-403 (OFF PART: PN&NBSP;<SPAN>1519M89P31</SPAN><SPAN>, SN&NBSP;</SPAN><SPAN>ECDD6130</SPAN><SPAN>). DMI REMAINS OPEN.</SPAN></P><P>LP&NBSP;822363 - M3: PERFORMED IGNITION SYSTEM AUDIBLE TEST IAW AMM 74-00-00. OPS CHECK GOOD. PERFORMED ENGINE RUNS IAW AMM 71-00-00. OPS CHECK GOOD. THIS CLEARS MDDR 124988.</P><P>LP&NBSP;822366:&NBSP;RE-OPENED&NBSP;MDDR 124988, CAT 'C', IAW MEL 74-00-01.</P><P>LP 822374:&NBSP;<SPAN>REMOVED AND REPLACED IGNITION CONTROL PANEL IAW AMM 80-11-51. OPS CHECK GOOD. ALSO PERFORMED IGNITION AUDIBLE TEST IAW AMM 74-00-00. OPS CHECKED GOOD. THIS CLEARS MDDR 124988. PLACARDS REMOVED.&NBSP;</SPAN></P>)

Part: IGNITER — FAILED (LT ENGINE) · airframe 102,535 hrs · 19,883 cycles

L ENGINE FAILED TO START 1ST ATTEMPT, STATUS MSG L ENG IGNITOR 2 , ENG START BOTH , 2ND ATTEMPT SUCCESSFUL.(<P>TRANSFERRED TO MDDR #124953 I.A.W MEL 74-00-01B CAT C&NBSP;</P><P>LOG PAGE 822355: TROUBLE SHOT IAW FIM 74-00 FAULT TREE 811. FOUND #2 IGNITOR TO BE AT FAULT. REMOVED AND REPLACED #2 IGNITOR IAW B767 AMM 74-21-02. PERFORMED AUDIBLE TEST IAW 74-00-00, OPS GOOD. THIS CLEARS MDDR #124953.</P>)

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 102,513 hrs · 19,875 cycles

DURING LEFT ENGINE START NO EGT RISE, NO FUEL FLOW RISE. FOLLOWED FCOM VOL 1 PROC. (WAIT 30 SECOND, SWITCH ENGINE START TO BOTH. TRY SECOND ATTEMPT) ENGINE START WAS SUCCESSFUL ON SECOND ATTEMPT. IGNITER WAS LEFT ON BOTH FOR REMINDER OF FLIGHT.(<P>PERFORMED LEFT ENGINE IGNITION SYSTEM AUDIBLE TEST, OPS NORMAL. ATTEMPTED TWO SUCCESSFUL ENGINE STARTS, NORMAL START AND IDEAL PARAMETERS FOUND WITHIN LIMITS IAW 74-00-00-705-104.</P>)

Part: IGNITER — FAILED (RT ENGINE) · airframe 102,478 hrs · 19,864 cycles

STATUS MESSAGE "R ENG IGNITOR 2".(<P>ITEM TRANSFERRED TO MDDR #124654 IAW MEL 74-00-01A, CAT A, DUE DATE 15FEB20. TIME AND INITIALS 0327Z ACL.</P><P>LP 1185158, ITEM M4: REMOVED AND REPLACED R/H ENGINE #2 IGNITOR PLUG IAW AMM 74-21-02. PERFORMED IGNITOR SYSTEM AUDIBLE TEST RIGHT ENGINE IAW AMM 74-00-00, ALSO PERFORMED ENG RUN IAW 71-00-00, OPS CHECK GOOD. THIS CLEARS MDDR #124654, PLACARD REMOVED. DISPATCH: ZH 14:08Z.</P>)

Part: O-RING — LEAKING (APU OIL SYSTEM) · airframe 102,483 hrs · 19,865 cycles

APU LEAKING OIL (LUBE FILTER HOUSING, OIL CAP)(<P>M4: REMOVED AND REPLACED FILTER O RING IAW AMM 49-27-03. LEAK CHECK GOOD AT THIS TIME. FILTER AND APU GOOD UPON INSPECTION.</P><P>M5: REMOVED AND REPLACED OIL CAP O-RING IAW AMM 12-13-04 AFTER REPLACEMENT OF LUBE HOUSING PACKING, REF ITEM 4, AND OIL CAP O RING OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME (OFF PART: P/N :A53204-221, S/N : NSN)</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 102,451 hrs · 19,859 cycles

APU OIL LOW @ .75.(<P>VERIFIED APU IS SERVICED TO FULL, EICAS INDICATION READ .75. TRANSFERRED TO DMI 124542 IAW MEL 49-94-01B CAT "D", DUE 10JUN2020, MAINTENANCE ACTION C/W.</P><P>LP&NBSP;1185176 - ITEM M4: APU OIL SERVICED TO REQUIRED QUANTITY PER AMM 49-11-00 AND OPERATION CHECK CARRIED OUT. OIL QUANTITY INDICATION GOOD AS REQUIRED. THIS CLEARS MDDR 124542.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 102,445 hrs · 19,856 cycles

RT ENGINE ANTI-ICE VALVE NOT IN COMMANDED POSITION.(<P>PERFORMED OPS CHECK ON RT ENG ANTI-ICE VALVE IAW AMM REF 30-21-00. OPS CHECKED GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 102,414 hrs · 19,844 cycles

2 CONSECUTIVE FLIGHTS, 'LT PACK TEMP' EICAS MSG SHOWN INTERMITTENTLY. PERFORMED SYS OPS TEST IAW B767 AMM 21-61-00 AND CHECKED CONDITION OF CONNECTIONS ON LEFT PACK COMPONENTS, OPS CHK GOOD AND ALL ELEC CONNECTORS SECURE. NO FAULTS FOUND AT THIS TIME.

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 102,407 hrs · 19,840 cycles

RADAR INOPERATIVE. TROUBLESHOT THE WX RADAR IAW AMM 34-00 AND FIM 34-43 FT 805. NO FAULT FOUND AT THIS TIME. SYS OPS CHECK GOOD.

Part: EXCITER — INOPERATIVE (LT ENGINE) · airframe 102,402 hrs · 19,838 cycles

LEFT ENGINE #2 IGNITION INOP.(<P>TRANSFERRED TO MDDR 124065, PER MEL 74-00-01B, CAT 'C', DUE DATE: 08FEB20.&NBSP; </P><P>LP 1178279: REMOVED AND REPLACED LH ENG #2 IGNITION EXCITER IAW AMM 74-11-01, OPS CHECK GOOD, THIS CLEARS DMI #124065, MCC NOTIFIED, PLACARDS REMOVED.</P>)

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 102,392 hrs · 19,833 cycles

LEFT ENGINE DID NOT LIGHT OFF, FIRST ATTEMPT. ENGINE START BOTH SELECTED AFTER MOTORING. SECOND ATTEMPT SUCCESSFUL. PERFORMED IGNITION SYSTEM AUDIBLE TEST IAW AMM 74-00-00. BOTH CHANNELS FOR BOTH IGNITORS ARE STRONG. NO DEFECTS NOTED. PERFORMED ENGINE RUN IAW AMM 71-00-00. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 102,398 hrs · 19,836 cycles

LEFT ENGINE, NO LIGHT OFF, SECOND ATTEMPT SUCCESSFUL. PERFORMED AUDIBLE TEST IAW AMM 74-00-00. OPS CHECKED NORMAL.

Part: RADAR — NO TEST (LT WX SYSTEM) · airframe 102,390 hrs · 19,832 cycles

DURING MX PRE-FLIGHT, LT AND RT WEATHER SPIKE DURING TEST USING SYS 1, SWAPPED RT'S, ISSUE FOLLOWED, UNSWAPPED, SYS 2 OPS SATISFACTORY. REMOVED AND REPLACED THE LT WEATHER RADAR IAW AMM 34-43-01. OPS TESTED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 102,360 hrs · 19,820 cycles

LEFT PACK TEMP EICAS MESSAGE. PERFORMED BITE TEST OF LEFT PACK TEMP CONTROL UNIT IAW FIM 21-51 FT 877. NO FAULTS NOTED.

Part: APU — UNKNOWN · airframe 102,331 hrs · 19,805 cycles

APU INOPERATIVE. PERFORMED AN OPS CHECK OF THE APU SYSTEM, RUNNING ENGINE AND AC LOAD IAW 71-00-00. ALL SYSTEMS PASSED TWO TIMES AND NO AUTO SHUTDOWN.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 102,332 hrs · 19,806 cycles

WX SYSTEM 1 INOP. PERFORMED FIM TASK 34-43 FAULT TREE 805, THE WXR SYSTEM IS OK.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 102,312 hrs · 19,797 cycles

APU SHUT DOWN PRIOR TO PUSHBACK AND WOULD NOT RESTART. TRANSFERRED TO MDDR 123361 AS PER DDG 49-11-01A, CAT "C", DUE 23JAN2020. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05. OPS TEST OK. THIS CLEARS DMI 123361.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 102,307 hrs · 19,795 cycles

DURING ENGINE START PROCEDURES, RIGHT FWD FUEL PUMP EICAS MESSAGE AND PRESS LIGHT WHEN SWITCH TURNED ON. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-42-01. OPS TESTED OK, LEAK CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,290 hrs · 19,789 cycles

R FWD FUEL PUMP EICAS CAUTION ILLUMINATED WHEN FUEL PUMP WAS TURNED ON FOR ENG START.(<P>CYCLED R FWD FUEL PUMP SW, LIGHT WENT OUT AND STAYED OUT IAW AMM CH 28-42-01. NO OTHER ISSUE NOTED IAW MM CH 28-22-00.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 102,264 hrs · 19,779 cycles

APU OIL QTY STATUS MESSAGE IN FLIGHT, "ADD" INDICATED FOR OIL QTY IN STATUS PAGE.(<P>SERVICED APU TO "FULL", OK TO CONTINUE IAW AMM 49-11-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (PIMU) · airframe 102,258 hrs · 19,776 cycles

RIGHT PIMU ON EICAS MESSAGE. PERFORMED SATISFACTORY TEST OF THE RIGHT PIMU, NO FAULTS FOUND. EICAS MESSAGE CLEARED, SYSTEM GOOD IAW FIM 71-01 FT 810.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 102,204 hrs · 19,738 cycles

AUX PITOT ADVISORY MESSAGE ON EICAS IN FLIGHT.(<P>PERFORMED FIM 30-31-43-824. NO FAULTS NOTED.&NBSP;</P>)

Part: B-NUT — LOOSE · airframe 102,181 hrs · 19,722 cycles

APU OIL QUANTITY AT 0.50. NO ADD OIL QUANTITY MESSAGE.<P><BR></P>(<P>PERFORMED VISUAL INSPECTION AFTER SERVICING, FOUND LOOSE B NUTS AT FUEL FILTER LOCATION SOLID LINE. TIGHTENED B NUTS PER AMM 20-11-00. OPS CHECKED APU PER AMM 49-11-00, OPS CHK AND LEAK CHK GOOD, OIL QUANTITY AT FULL.</P>)

Part: B-NUT — LEAKING (APU OIL SYS) · airframe 102,175 hrs · 19,718 cycles

APU AUTO-SHUTDOWN DUE TO LOW OIL.(<P>UPON INVESTIGATION, FOUND LOOSE B-NUT LEAKING OIL. TIGHTENED B-NUT IAW B767 AMM 20-11-00. OPS CHECK OF APU IAW B767 AMM 49-11-00, OPS CHECK GOOD AND NO LEAKS FOUND. (NOTE: SERVICED APU WITH 03 QTS OF OIL).</P><P>(NOTE 2 - APU COLD SOAK START NOT REQUIRED DUE STARTING CKT OK. APU STARTING OPERATION OK)&NBSP;</P>)

Part: PITOT TUBE — NOT REPORTED (LT AUX) · airframe 102,156 hrs · 19,707 cycles

LEFT AUX PITOT. REMOVED AND REPLACED LT AUX PITOT PROBE ASSY IAW AMM 34-11-01. OPS CHECK GOOD IAW AMM 30-31-00.

Part: SEAL — BROKEN (FIRST AID KIT) · airframe 102,119 hrs · 19,689 cycles

FOUND AIRLINE FIRST AID KIT WITH SEAL BROKEN.(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03.<BR /></P>)

Part: CONTAINMENT BAG — MISSING (CABIN) · airframe 102,034 hrs · 19,663 cycles

PED FIRE CONTAINMENT BAG MISSING FROM LOCATION SUPERNUMERARY SEAT.(<P>TRANSFERRED TO MDDR 120319 PER MEL 25-20-01, CAT 'E'.&NBSP; NEW NEF ITEM.</P><P>LP 1105703:&NBSP;INSTALLED AIRCRAFT PED FIRE CONTAINMENT BAG IAW EO 6725A212. THIS CLEARS DMI #120319. PLACARD REMOVED.<BR /></P>)

Part: BLADE — DAMAGED (NR 1 ENG FAN) · airframe 101,913 hrs · 19,621 cycles

#5 FAN BLADE ON #1 ENG HAS SMALL DAMAGE.(<P>REPAIRED #5 FAN BLADE IAW AMM 72-31-02-308-045-1100.&NBSP;</P><P>LP 1223620 - M9: FPI REQUIRED FOR L/H ENG, #5 BLADE. PERFORMED FPI OF #5 BLADE TIP BLEND IAW B767 AMM 70-11-06, NO DEFECTS NOTED.</P><P>LP 1223621 - M11:&NBSP;OPS CHECK GOOD, CLEAR TO RETURN TO SERVICE.&NBSP;</P>)

Part: BLADE — DAMAGED (LT ENG FAN) · airframe 101,913 hrs · 19,621 cycles

FOUND LH ENG BLADES (FAN) #10 &AMP; 11 LEADING EDGE TIP CURL.(<P>LP 1223619 - M5: REF LP 1223618 - M3. REMOVED FAN BLADES #9, 10, 11, 4, 5, AND 6 IAW AMM 72-31-02. RE-INSTALLED BLADES #4, 6, AND 9 ON L/H ENG IAW AMM 72-31-02.</P><P>LP 1223618 - M3:&NBSP;REMOVED AND REPLACED LH ENG BLADE #10 IAW AMM 72-31-02, OPS CHECK GOOD. CLEAR TO RETURN TO SERVICE. OFF PART (PN:&NBSP;1338M51P06, SN:&NBSP;MTJ47813)</P><P>LP 1223621 - M10: REMOVED AND REPLACED LH ENG BLADE #11 IAW AMM 72-31-02, OPS CHECK GOOD. CLEAR TO RETURN TO SERVICE.&NBSP;</P><P>LP 1223621 - M12: DUE TO FAN BLADE REPLACEMENT, L/H ENG REQUIRES VIBE SURVEY. C/W TEST NO. 6 VIBRATION SURVEY IAW 71-00-00, TEST SUCCESSFUL.&NBSP;</P>)

Part: START VALVE — UNKNOWN (RT ENGINE) · airframe 101,845 hrs · 19,594 cycles

RIGHT ENGINE START VALVE LIGHT INOPERATIVE. PERFORMED OPERATIONAL TEST IAW AMM 71-00-00/201, OPS CHECKED GOOD.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 101,823 hrs · 19,585 cycles

LEFT PACK INOPERATIVE. PERFORMED BITE TEST, NO FAULTS FOUND. RESET LT PACK. OPS CHECKED GOOD AT THIS TIME IAW FIM 21-51 FT 803. PERFORMED T/S PER FIM 21-51 FT 811, REQUIRES REPLACEMENT OF THE FLOW CONT. AND SHUTOFF VALVE. NO CONTINUITY AT 02770. REMOVED AND REPLACED FLOW CONTROL VALVE IAW AMM 21-51-01. OPS CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN CARGO BAY) · airframe 101,804 hrs · 19,578 cycles

MAIN CARGO LOOP 1 STATUS MESSAGE AFTER MULTIPLE MAIN CARGO WARNING EICAS MESSAGES. ERFORMED BITE PROCEDURE FOR CARGO SMOKE DETECTION IAW FIM 26-14 F/T 809.&NBSP; OPS CHECK GOOD. CREW REPORTS NO CARGO SMOKE/FIRE INDICATION DURING FLT. REMOVED AND REPLACED MAIN CARGO DECK SMOKE DETECTOR IA2F IAW B767 BCF 26-14-01. OPS CHECK GOOD.

Part: VALVE — UNKNOWN · airframe 101,793 hrs · 19,574 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01 OPERATIONAL CHECK NORMAL.

Part: FIRE DETECTOR — MALFUNCTIONED (MAIN CARGO) · airframe 101,789 hrs · 19,573 cycles

AFTER OPENING MAIN CARGO DOOR, MAIN CARGO FIRE ILLUMINATED WITH MAIN CARGO FIRE EICAS MESSAGE. THE MESSAGE WENT OUT, THAN RE-ILLUMINATED, NO SMOKE OR FIRE DETECTED.&NBSP; &NBSP;(<P>T/S PER FIM 26-14 FT 809 AND 803, NO FURTHER FAULTS NOTED AT THIS TIME.&NBSP;</P>)

Part: FIRE WARNING — FALSE ACTIVATION (CARGO DECK) · airframe 101,785 hrs · 19,572 cycles

CVG PRIOR TO COMPLETION OF LOADING , MULTIPLE MAIN CARGO DECK FIRE WARNINGS , NONE IN FLIGHT, NOTED BY MX OPS CHECKED GOOD IAW AMM 26-10-00.

Part: FIRE WARNING — FALSE ACTIVATION (FWD CARGO) · airframe 101,785 hrs · 19,572 cycles

FWD CARGO FIRE WARNING ON THE GROUND. PERFORMED FWD CARGO FIRE WARNING I.A.W AMM 26-16-00. NO DEFECTS NOTED.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 101,753 hrs · 19,559 cycles

WXR SYS STATUS MSG; WX INOP ON BOTH SYS 1 AND SYS 2.(<P>AFTER INSPECTION OR WX RADAR SYSTEM, FOUND SYSTEM #1 AND SYSTEM #2 C/B'S POPPED OUT. RESET C/B'S AND PERFORMED WX RADAR OPS CHECK IAW AMM 34-43-00, OPS TEST NOW SATISFACTORY.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 101,746 hrs · 19,556 cycles

MAIN CARGO LOOP STATUS MESSAGE. TRANSFERRED TO MDDR # 118203 IAW MEL 26-16-02-01, CAT C. COMPLIED WITH MX PROCEDURE. MCC NOTIFIED AND PLACARDS INSTALLED. LP 1111426 - M9: PERFORMED FIM 26-14 FT 809 BITE PROCEDURE AND NO FAULTS NOTED. OPS CHECK NORMAL. THIS CLEARS MDDR #118203. PLACARDS REMOVED AND MCC NOTIFIED.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 101,744 hrs · 19,555 cycles

WINDOW HEAT, RIGHT FWD SWITCH WON'T STAY ENGAGED. REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW AMM 30-41-02. OPS CHECK GOOD AT THIS TIME, NO FURTHER DEFECTS NOTED.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 101,713 hrs · 19,543 cycles

#2 ENGINE, #10 FAN BLADE NICKED ON LEADING EDGE AREA "D". BLENDED #2, ENG #10 FAN BLADE LEADING EDGE IAW AMM 72-31-02. INSPECTED BLADE, NO CRACKS NOTED. REQUIRES DYE PENETRANT INSPECTION TO NON MEL 117872. LP 1111411 - M4: COMPLETED THE FLUORESCENT PENETRANT INSPECTION ON THE NUMBER 2 ENGINE, NUMBER 10 FAN BLADE PER AMM 70-11-06-232-001-H00. NO ITEMS FOUND. THIS CLEARS DMI 117872. MCC NOTIFIED.

Part: MOTOR — FAILED (AC BAY) · airframe 101,660 hrs · 19,524 cycles

STATUS MESSAGE CABIN ALT AUTO 1. PERFORMED FIM 21-31 FT 803. FOUND AC MOTOR FAULT. P/N 2022480-9 ON ORDER WITH MCC. NO FURTHER DEFECTS. TRANSFERRED TO MDDR 117554 IAW DDG 21-31-01A CAT "C" DUE: 20SEP2019. LP 1102938 - M4: REMOVED AND REPLACED #1 OUTFLOW VALVE ACT AC MOTOR IAW AMM 21-31-05 OPS CK GOOD NO MSG OR DEFECTS NOTED. OFF PART (PN;2022478-4, SN:42-266). LP 1102940 - ITEM 1: CABIN ALT 1 STATUS @ APPROX 36,000 FT, 1.5 HR AFTER TAKEOFF. RE-OPENED MDDR 117554 PER MEL 21-31-01A. LP 1076205 - M10:&NBSP;PERFORMED T/S IAW FIM 21-31 FT 809. STEP 27 NEEDS CONTROLLER AC RETURNED TO NORMAL CONFIG. DMI 117554 REMIANS OPEN. LP 1076207 - M3: T/S PER FIM 21-31, FAULT TREE 803. FOUND BAD #1 AC MOTOR. SUSPECT WRONG MOTOR WAS CHANGED. P/N - 2022478-4. SWAPPED CONNECTOR ON MOTOR 1 & 2, CONFIRMED MOTOR #1 BAD. DMI # 117554 REMAINS OPEN. LP 1076210 - M4: REMOVED AND REPLACED #1 AFT AC MOTOR ACTUATOR ASSY PER AMM 21-31-04. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 117554. PLACARDS REMOVED AND MCC NOTIFIED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 101,655 hrs · 19,522 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. PERFORMED AUTO CABIN PRESS CONTROLLER BITE CHECK NO FAULTS NOTED MSG EXTINGUISHED NO FURTHER DEFECTS NOTED BITE CHECK GOOD IAW AMM 21-31-00.

Part: RELAY — FAILED (ANIT-ICE SYS) · airframe 101,606 hrs · 19,504 cycles

R ENG ANTI ICE EICAS MSG. COMPLIED W/ PROCEDURE, MESSAGE REMAINS. REMOVED AND REPLACED RT ENG ANTI ICE VALVE PER AMM 30-21-03. NO HELP, FURTHER TROUBLESHOOTING REQUIRED. OFF PART (PN: 2790583-108, SN: 4104F) LP 846183 - M5: REMOVED AND REPLACED K649 RELAY REF WDM 30-21-01. RAN ENGINE TAI, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (APU) · airframe 101,599 hrs · 19,502 cycles

APU BATTERY REQUIRES CHANGING. REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (MAIN) · airframe 101,599 hrs · 19,502 cycles

MAIN BATTERY DISCHARGED. REMOVED AND REPLACED MAIN BATTERY IAW AMM 24-31-01, OPS CHECK GOOD.

Part: FILTER — NOT REPORTED (PNEUMATIC SYS) · airframe 101,584 hrs · 19,500 cycles

REPLACE PNEUMATIC HP CONTROLLER AIR FILTER. REPLACED PNEUMATIC HP CONTROLLER AIR FILTER IAW AMM 36-11-08-004-028-007 & AMM 36-11-08-004-032-007. CONDITION CHECKS NORMAL.

Part: TRAY — CORRODED (BS 654) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FWD CGO ROLLER TRAY CORROSION AT STA 654+88, RBL 20.(<P>REPAIRED THE CORROSION AREA IAW SRM 53-00-53-2R-1 REV.110 AND EI NO T2019A53M-3086 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL. ORIGINAL EI ATTACH ON W/O NO 3434859.</P>)

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT CHANNEL, BULK CGO COMPARTMENT SUPPORT CHANNEL STA 1415 TO STA 1540, RBL 42.(<P>REMOVED&NBSP;DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS WITH FASTENERS IAW SRM 51-40-02-0G-0 REV 110, DWG 146T5002 SH 1 REV E, DWG 146T5002 SH 3 REV. G, AND DWG 146T5002 SH 4 REV C. JOB COMPLETED AND CONDITION CHECKS NORMAL.

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT STATION 1415 TO STA 1540, RBL 7.9. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG NO 146T5002 SH 1 REV E. CONDITION CHECKED NORMAL.

Part: FILTER — NOT REPORTED · airframe 101,584 hrs · 19,500 cycles

REPLACE PNEUMATIC PRESSURE CONTROLLER AIR FILTER. REPLACED THE AIR FILTER IAW AMM 36-11-19-004-027 & AMM 36-11-19-404-032. CONDITION CHECK NORMAL.

Part: CLAMP — WORN (FIRE DETECTOR) · airframe 101,584 hrs · 19,500 cycles

FOUND FIRE DETECTOR CLIP ONE EACH ON LT & RT W/W NEAR BS 977 WORN. IAW AMM REV127 26-17-01-024-001 REMOVED THE FIRE DETECTION FOR LT & RT W/W FIRE DETECTION CLAMPS REPLACEMENT. REMOVED DAMAGE CLAMP IAW SRM 51-40-02-0G-0 REV.110.INSTALL NEW CLAMP WITH FASTENERS IAW SRM 51-40-02-0G-0 REV 110 AND AIPC 53-51-52-01 NEW CLAMP AND NEW CONDITION CHK NML. IAW AMM REV129 26-17-00-715-010 REV 127 PEM W/W FIRE DETECTION OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY</SPAN></P>)

Part: BEARING — WORN (ROD END) · airframe 101,584 hrs · 19,500 cycles

WORN-END BEARING, #1 ENG L/H CORE COWL HOLD OPEN ROD.(<P>REPLACED COWL HOLD OPEN ROD END BEARING WITH NEW IAW 70-50-00-912-001. CONDITION CHECK NORMAL.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>LOCKING&NBSP;OFF PART (PN:&NBSP;NAS1193K5C<SPAN>)</SPAN></P>)

Part: WARNING LIGHT — FALSE ACTIVATION (IDG) · airframe 101,584 hrs · 19,500 cycles

IDG QAD COUPLING-CHECK TORQUE AND CONDITION. PFM QAD COUPLING TORQUE CHECK. RESULT NORMAL.

Part: FRAME — CORRODED (BS 1109) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND FRAME CORRODED AT BS 1109, STRINGER 17L. REPAIRED THE FRAME IAW EI T2019A53M-2786, REV 1.

Part: BRACKET — WORN (NR 2 NACELLE) · airframe 101,584 hrs · 19,500 cycles

WORN BRACKET, #2 ENG BOTH FAN COWL FWD HOLD OPEN ROD SUPPORT.(<P>REPLACED FAN COWL FWD HOLD OPEN ROD SUPPORT BRACKET WITH NEW IAW 70-50-00-912-001. CONDITION CHECK NORMAL.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>SPLIT PIN OFF PART (PN: MS24665-155)</P><P>BUSHING OFF PART (PN: NAS77-4-18)</P><P>WASHER OFF PART (PN: S700W0125-001)</P>)

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

SUPPORT CHANNEL, BULK CARGO COMPARTMENT, BS 1415 - 1540, BL 0 CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV. 110. INSTALLED NEW SUPPORT CHANNEL WITH FASTENERS IAW SRM 51-40-02-0G-0, DWG 146T5002 SH 2 REV F, DWG 657T5102 SH 6 REV A, DWG 146T5002 SH 5 REV C.

Part: NUT PLATE — DAMAGED (NR 1 EXHAUST) · airframe 101,584 hrs · 19,500 cycles

DAMAGE NO.1 ENG EXHAUST SLEEVE NUTPLATE DAMAGE AT 9 O'CLOCK(<P>REMOVE DAMAGED NUTPLATE IAW SRM 51-40-02-0G-0 REV.110. INSTALLED NEW NUTPLATE IAW SRM 51-40-02-0G-0 REV 110 AND BOEING DWG 314U2100 5H6 REV.N. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: PACKING — LEAKING (OIL SUMP) · airframe 101,584 hrs · 19,500 cycles

FOUND ENG SN: 707422 LPT D-SUMP COVER OIL SEEPING EXIST.(<P>REPLACED D-SUMP COVER PACKING WITH NEW PART IAW 71-00-00-795-034. PERFORMED ENG IDLE LEAK CHECK. RESULT CONDITION CHECK NORMAL AND NO LEAK FOUND IAW&NBSP;AMM&NBSP;<SPAN>72-53-02-004-001 &AMP; AMM 72-53-02-404-004</SPAN></P>)

Part: FRAME — CRACKED (BS 923) · airframe 101,584 hrs · 19,500 cycles

FOUND FRAME CRACKED APPROX 0.2" AT BS 923.7, WL 197. ACCOMPLISHED EI T2019A53M-2681 REV. 1. CONDITION CHECKED NORMAL AND JOB COMPLETED.&NBSP;</P>)

Part: FILTER — NOT REPORTED (IDG HEAT EXCHANG) · airframe 101,584 hrs · 19,500 cycles

REPLACE OR CLEAN THE IDG EXCHANGE AIR SHUTOFF VALVE FILTER. PERFORM IDG HEAT EXCHANGE AIR SHUTOFF VALVE FILTER REPLACEMENT IAW AMM 24-11-07-202-016, REV 127. CONDITION CHECKED NORMAL.

Part: PIN — DAMAGED (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

DAMAGE GUIDE PIN #1 PYLON L/H FAN COWL SUPPORT BEAM HINGE AT FIRST AND THIRD POSITION TOTAL 2 EA(<P>REPLACE 1L FAN COWL SUPPORT BEAM FIRST AND THIRD HINGE PIN WITH NEW IAW&NBSP;<SPAN>AMM 71-11-04-712-011 &AMP;&NBSP;</SPAN><SPAN>AMM 71-11-04-712-012</SPAN></P>)

Part: SCREEN — DAMAGED (COOLING FAN) · airframe 101,584 hrs · 19,500 cycles

FOUND E/E COOLING SYS SUPPLY FAN SCREW DAMAGED. REPLACED THE SCREEN OF THE SUPPLY FAN IAW AMM 21-58-22-002-047 & AMM 21-58-22-002-039.

Part: RIVET — LOOSE (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

LOOSEN RIVET. NO.1 ENG L/H CORE COWL L/E WEAR STRIP(<P>REPLACE DAMAGE RIVETS WITH NEW RIVETS&NBSP; IAW SRM 51-40-02-0G-0 REV110 AND GOODRICH CMM 71-13-23 REV.4.1 JOB COMPLETED AND COND CHK NML</P>)

Part: CHECK VALVE — NOT REPORTED (FWD CARGO) · airframe 101,584 hrs · 19,500 cycles

FOUND E/E COOLING SUPPLY FAN CHECK VALVE AT FWD CARGO. REPLACED THE SUPPLY FAN CHECK VALVE IAW&NBSP;<SPAN>AMM 21-58-02-004-075&NBSP;&NBSP;</SPAN><SPAN>AMM 21-58-02-404-076</SPAN></P>)

Part: SUPPORT ANGLE — CORRODED (BS 610-632) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT ANGLE, FWD CGO FLOOR STRUCTURE STA 632 TO STA 610, RBL 31. REMOVEDDAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV.110 AND DWG 143T5012 SH 3 REV G.

Part: WARNING LIGHT — FALSE ACTIVATION (IDG OIL FILTER) · airframe 101,584 hrs · 19,500 cycles

IDG FILTER- CHECK OIL FILTER PRESSURE INDICATOR POSITION. EXAMINED OIL FILTER PRESSURE INDICATOR POSITION. RESULT NORMAL.

Part: TEE FITTING — CRACKED (BS 287 NLG WW) · airframe 101,584 hrs · 19,500 cycles

CRACK -TEE, NOSE WHEEL WELL BULKHEAD VERTICAL TEE LH SIDE AT STA 287, BL 25, WL 172.(<P>PERFORMED CRACK AREA REPAIR IAW EO NO 6753A027 PART 3 AND SRM 51-70-12-0G-0 REV 110. JOB COMPLETED AND&NBSP;CONDITION CHECKS NORMAL.</P>)

Part: LANYARD — CHAFED (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

CHAFING LANYARD NO.1 ENG NOSE COWL AFT BULKHEAD NEAR 7 O'CLOCK POSITION&NBSP;(<P>REPLACE NO 1 ENG NOSE COWL AFT BULKHEAD LANYARD WITH NEW PARTS</P>)

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 101,584 hrs · 19,500 cycles

NR 3 SLAT DAMAGED, OUTBOARD NOSE SKIN RIVET SURROUND MINOR CRACK DAMAGE OSS 792. REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REVISION 110. CONDITION CHECKED NORMAL.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 101,584 hrs · 19,500 cycles

START VALVE NOT FULLY OPEN DURING ENG RUN TEST, LT ENGINE. REPLACED THE LT ENG START VALVE IAW AMM 80-11-02-004-001 & AMM 80-11-02-004-017.

Part: BOLT — WORN (THRUST REVERSER) · airframe 101,584 hrs · 19,500 cycles

WORN-#2 ENG BOTH T/R OPENING ACTUATOR UPPER HINGE BOLT WORN.(<P>REPLACED BOTH T/R OPENING ACTUATOR UPPER HINGE BOLTS WITH NEW IAW 78-31-06. OPEN AND CLOSED THE T/R. CHECK RESULT NORMAL. IAW AMM&NBSP;<SPAN>78-31-06-004-001 &AMP; AMM&NBSP;</SPAN><SPAN>78-31-06-404-006</SPAN></P><P><SPAN><BR DATA-MCE-BOGUS="1" /></SPAN></P><P><SPAN>WASHER OFF PARTS (PN: 9132M39P01, PN:&NBSP;NAS1149C0463R)</SPAN></P><P><SPAN>NUT OFF PART (PN:&NBSP;NAS1291C4M)</SPAN></P>)

Part: ANGLE — CORRODED (BS 1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

ANGLE CORRODED, BULK CARGO COMPARTMENT, LOWER SIDE ANGLE BS 1540, RBL 0 TO RBL 32. REMOVED DAMAGE PARTS IAW SRM 51-40-02-02-0G-0 REV.110. FABRICATED NEW ANGLE IAW EI T2019P53M-2874 REV.0. INSTALLED THE NEW ANGLE WITH FASTENERS IAW SRM 51-40-02-0G-0 REV.110, DWG. 453T1304, SH2, REV 0, AND DWG 453T1311, SH1. CONDITION CHECKED NORMAL.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 101,584 hrs · 19,500 cycles

CRACKED SKIN, OSS 871.63, RT WING NR 11 SLAT, UPPER SURFACE. REPAIRED THE AREA IAW SRM 57-43-01-2R-2, REPAIR 2 REV. 110. CONDITION CHECKED NORMAL.

Part: ANGLE — CORRODED (BS 977) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND M/D BS 977, S-14.5L BRACKET CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. FABRICATED NEW ANGLE IAW EI T2019P53M-2879, REV 0. INSTALLED A NEW ANGLE WITH FASTENERS IAW SRM 51-40-02-0G-0, REV 110, AND DWG 145T1308, SH 7, REV A. CONDITIONS CHECKED NORMAL.

Part: RUB STRIP — BROKEN (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

BROKEN RUB STRIP NO.1 ENG NOSE COWL AFT BULKHEAD OUTER RING NEAR 8 O'CLOCK POSITION(<P>REMOVE DAMAGED PARTS IAW GEK9250 SPM 70-13-01 REV.108. INSTALL NEW PARTS IAW GEK9250 SPM 70-13-01 REV.108 AND GOODRICH CMM 71-11-16 REV.46. JOB COMPLETED AND CONDITION CHECK NORMAL</P><P><BR /></P><P>RIVET PART OFF (PN: 201-120911-00-0101)</P>)

Part: DOOR FRAME — CORRODED (BS 123.7) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION ON THE FRAME CHANNEL OF L1 DOOR SURROUND AT DOOR STA 123.7 NEAR S-11L.(<P>PERFORMED CORROSION REPAIR ON THE FRAME CHANNEL OF L1 DOOR SURROUND AT DOOR STA 123.7,&NBSP; NEAR S-11L IAW EI NO: T2019A53M-2633 REV 1. JOB COMPLETED AND&NBSP;CONDITION CHECKS NORMAL.</P>)

Part: WIRE HARNESS — DAMAGED (LT FUEL TANK) · airframe 101,584 hrs · 19,500 cycles

FOUND L/H MAIN TANK WIRING HARNESS DAMAGED(<P>IAW AMM 28-41-09-004-001-002. 28-41-09-404-028-002, 28-41-004-036-002 AND 28-41-01-404-017-002 REV 127 REPLACED MAIN TANK WIRING HARNESS M02012. IAW AMM 28-41-00-735-049-002 REV129 PERFORMED FQIS SYSTEM TEST AND RESULT WAS SATISFACTORY</P>)

Part: RUB STRIP — LOOSE (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

LOOSEN RIVETS NO.1 ENG NOSE COWL AFT BULKHEAD OUTER RING RUB STRIP NEAR 6 O'CLOCK POSITION(<P>REPLACED DAMAGED PARTS WITH NEW IAW SRM 51-40-02-0G-0 REV110 AND GOODRICH CMM 71-11-16 REV 46. JOB COMPLETED AND COND CHK NML</P>)

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT AT STA 1415 TO STA 1540, RBL 36.5.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG NO: 146T5002 SH 1 REV E. JOB COMPLETED AND CONDITION CHECK NORMAL.&NBSP;</P>)

Part: BRACKET — WORN (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

BRACKET WORN, NR 1 PYLON PRV R/H PNEUMATIC DUCT SUPPORT LINK. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV.110 AND DWG 311T2150 SH 5, REV 0.

Part: STRINGER — CORRODED (BS 1197-1219) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND BS 1197+132, STRINGER 17R CORRODED. REPAIRED THE STRINGER IAW EI T2019A53M-2637 REV 1. CONDITION CHECKED NORMAL.

Part: FILTER — DIRTY (STARTER VALVE) · airframe 101,584 hrs · 19,500 cycles

STARTER VALVE PNEUMATIC FILTER CLEAN AND REINSTALL(<P>PFM ESN 707422 STARTER VALVE FILTER CLEAN IAW AMM 80-11-04-002-001 &AMP; AMM 80-11-04-112-019.</P>)

Part: ROD END — WORN (LT NACELLE) · airframe 101,584 hrs · 19,500 cycles

WORN - #2 ENG L/H CORE COWL SUPPORT ROD END AND WELD ASSY WORN.(<P>REPLACED #2 ENG L/H CORE COWL SUPPORT ROD END AND WELD ASSY WITH NEW IAW 70-50-00-912-001. CONDITION CHECK NORMAL.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>SPACER OFF PART (PN: NAS43HT5-8)<BR DATA-MCE-BOGUS="1" /></P><P>BEARING END ROD OFF PART (PN: 26C0313-11)</P><P>LOCKING OFF PART (PN: NAS1193K5C)</P>)

Part: PACKING — LEAKING (BEARING MANIFOLD) · airframe 101,584 hrs · 19,500 cycles

FOUND ENG SN:707422 NO. 1 BEARING MANIFOLD OIL LEAK.(<P>REPLACED NO. 1 BEARING MANIFOLD PACKING. PERFORMED ENG IDLE RUN LEAK CHECK. RESULT CONDITION CHECK NORMAL AND NO LEAK FOUND IAW 72-31-03-004-001 &AMP; 72-31-03-404-005.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PACKING OFF PART (PN: R1316P004)<BR DATA-MCE-BOGUS="1" /></P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: INLET — SCRATCHED (NR 1 ENGINE) · airframe 101,584 hrs · 19,500 cycles

SCRATCHES ON THE INLET, NR 1 ENG NOSE COWL, FROM 5 TO 7 O'CLOCK. REMOVED SCRATCH AND MEASURED THE REWORKED AREA; DEPTH = 0.003", LENGTH = 2.8", WIDTH = 1.2". IT IS WITHIN ALLOWABLE LIMIT IAW SRM 54-12-01-1A-1 DETAIL III REV. 110 AND JOB CARD ATTACHING SHEET CONTROL 0180939. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01-0G-0 REV. 110. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: MONITOR — NO TEST (RIGHT) · airframe 101,584 hrs · 19,500 cycles

FOUND R/H PIMU FUNCTIONAL FAIL CM01414(<P>IAW AMM 77-35-02-044-001-H00 &AMP; 27-35-02-404-006-HOO REV 127. REPLACED R/H PIMU CM01414. IAW AMM 77-35-02-404-006 H00 &AMP; 77-35-00-722-007 H00 REV 127. PERFORMED PIMU TEST AND THE RESULT WAS SATISFACTORY</P>)

Part: SHIM — MIGRATED (NR 2 NACELLE) · airframe 101,584 hrs · 19,500 cycles

MIGRATION - SHIM NO.2 ENG NOSE COWL THRM ANTI ICING DUCT NEAR 1 O'CLOCK POSITION(<P>REPLACED NO. 2 ENG NOSE COWL THRM ANTI ICING DUCT SEAL</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (IDG FILTER) · airframe 101,584 hrs · 19,500 cycles

IDG FILTER, CHECK OIL FILTER PRESSURE INDICATOR POSITION.(<P>PERFORMED OIL FILTER PRESSURE INDICATOR POSITION CHECK IAW 24-11-01-246-211 REV. 127. JOB COMPLETED AND CONDITION CHECK SATISFACTORY.&NBSP;</P>)

Part: DIODE — FAILED (SMOKE DETECTION) · airframe 101,584 hrs · 19,500 cycles

FOUND PII-5 C766, & PII-4 C772 CIRCUIT BREAKER TRIPPED. REPLACED THE CIRCUIT BREAKERS C766 & C772, RELATED DIODES R203 & R204 PER WDM 26-16-11 REV55 AND CONDITION CHK NORMAL, PFM LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM OPERATIONAL TEST IAW AMM 26-16-00-715-001 REV 127 AND RESULT WAS SATISFACTORY.

Part: RUB STRIP — WORN (NR 2 NACELLE) · airframe 101,584 hrs · 19,500 cycles

DAMAGE - WEAR STRIP, NO. 2 ENG NOSE COWL OUTER BARREL T/E AT 2-3 O'CLOCK POSITION. REMOVED DAMAGED PARTS IAW GEK9250 SPM 70-13-01 REV. 108. INSTALLED NEW PARTS IAW GEK9250 SPM 70-13-01 REV. 108 AND GOODRICH CMM 71-11-16 REV. 46. JOB COMPLETED AND CONDITION CHECKS NORMAL.

Part: SKIN — DENTED (NR 1 EXHAUST) · airframe 101,584 hrs · 19,500 cycles

DENT-OUTER SKIN NO.1 ENG EXHAUST SLEEVE NAC STA 346 NEAR 1 OCLOCK POSITION(<P>MEASURED THE EXHAUST SLEEVE DENT AREA LENGTH 0.2" WIDTH=0.2", DEPTH AND .0094", A/Y=0.2/.0094=21.28. WITHIN ALLOWABLE DAMAGE IAW SRM 54-42-30-1A-1 REV.110. JOB COMPLETED AND COND CHK NML</P>)

Part: SKIN — CORRODED (BS 1197) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND AFT CARGO UNDER FLOOR AREA CORROSION AT BS 1197+22 - 1197+44, S-36R TO S-37R. REMOVED THE CORROSION IAW SRM 51-10-02-0G-0 REV. 110. REPAIRED IAW EI T2019A53M-3220 REV. 1. CONDITION CHECK NORMAL.

Part: WIRE HARNESS — DAMAGED (RT WING) · airframe 101,584 hrs · 19,500 cycles

FQPU BITE TEST SHOW MSG R/H R/H&NBSP; HIZ WIRE LOW RESISTANCE(<P>IAW AMM 218-41-09-004-001-002 REV 127 AND AMM 28-41-09-404-028-002 REV129 REPLACED R/H WING FQIS WIRE CM0201372 IAW AMM 28-41-00-035-049-002 REV 127 PERFORMED FQIS SYSTEM TEST AND RESULT WAS SATISFACTORY</P>)

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 101,584 hrs · 19,500 cycles

OSS 792.54, WING NR 10 SLAT UPPER SURFACE SKIN CRACKED. REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV 110. CONDITION CHECKED NORMAL.

Part: SEAL — BROKEN (EXHAUST SLEEVE) · airframe 101,584 hrs · 19,500 cycles

BROKEN - SPRING SEAL #1 ENG EXHAUST SLEEVE NEAR 1 O'CLOCK POSITION QTY 2EA(<P>REPLACED NO 1 ENG EXHAUST SLEEVE SPRING SEAL WITH NEW</P>)

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT STA 1415 TO STA 1540, LBL 7.9. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 110. INSTALLED NEW SUPPORT CHANNEL WITH FASTENERS IAW SRM 51-40-02-0G-0, REV. 110, AND DWG 146T5002, SH 1, REV E.

Part: VALVE — MALFUNCTIONED (RT ENGINE) · airframe 101,584 hrs · 19,500 cycles

FOUND RT FAMV ALWAYS IN REGULATOR DURING ENG RUN. REMOVED AND REPLACED THE RT ENG FAN AIR VALVE IAW AMM 36-11-16-004-001 REV. 127. PERFORMED RT ENG FAN AIR VALVE OPERATIONAL TEST IAW AMM 36-11-16-404-015 REV. 127, OPS TEST NORMAL. CONDITION CHECKED SATISFACTORY.

Part: BOLT — WORN (THRUST REVERSER) · airframe 101,584 hrs · 19,500 cycles

WORN NO 1 PYLON R/H T/R OPEN ACTUATOR UPPER BOLT WORN(<P>REPLACED #1 PYLON R/H T/R OPEN ACTUATOR UPPER BOLT WITH NEW PARTS IAW&NBSP;<SPAN>AMM 78-31-06-004-001 &AMP;&NBSP;</SPAN><SPAN>AMM 78-31-06-404-006</SPAN></P>)

Part: RIVET — DAMAGED (NR 2 NACELLE) · airframe 101,584 hrs · 19,500 cycles

CHAFING SURFACE NO.2 ENG R/H CORE COWL INNER FACE AFT LATCH COVER(<P>REPLACE DAMAGE PARTS WITH NEW PARTS IAW SRM 51-40-02-05-G-0 REV.110 AND GOODRICH CMM 71-13-24 REV.44. JOB COMPLETED AND COND CHK NML

Part: FLOOR SUPPORT — CORRODED (BS 606-632) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FLOOR SUPPORT CORRODED, FWD CARGO COMPARTMENT, BS 544 TO 632, LBL 44. REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 REV 110, DWG 451T1504, SH4, REV. C, AND DWG 143T5010, SH17, REV E. CONDITION CHECKED NORMAL.

Part: TRAY — CORRODED (BS 610) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FWD CARGO ROLLER TRAY HAS CORROSION AT STA 610, RBL 6. REPAIRED THE CORROSION AREA IAW SRM 53-00-53-2R-1 REV 110 AND EI T2019A53M-3086 REV 1. CONDITION CHECKS NORMAL.

Part: STRUCTURE — CORRODED (WING) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND THAT OVERWING FILL PORT ON BOTH WINGS HAS CORROSION AROUND THE STRUCTURE.(<P>REPAIRED CORROSION AREA IAW EI NO T2019A57M-2788 REV 1. JOB COMPLETED AND&NBSP;CONDITION CHECK NORMAL.</P>)

Part: STRINGER SPLICE — CORRODED (BS 412-456) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

STRINGER SPLICE CORRODED, FWD CARGO COMPARTMENT, LOWER LOBE BS 429, STRINGER 39R. REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS WITH FASTENERS IAW SRM 51-40-02-0G-0 REV 110, DWG NO 140T0110 SH 30, AND 140T0110 SH 33.

Part: RIVET — SHEARED (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

SHEAR-PLASTIC RIVET NO.1 ENG NOSE COWL AFT BULKHEAD OUTER RING RUB STRIP, NEAR 5 O'CLOCK POSITION.(<P>REPLACED DAMAGED RIVET WITH NEW RIVET IAW GE SPM 70-13-01 REV.108 AND GOODRICH CMM 71-11-16 REV.46. JOB COMPLETED AND COND CHK NML</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (STARTER) · airframe 101,584 hrs · 19,500 cycles

STARTER CHIP DETECTOR, PERFORM A VISUAL INSPECTION. PERFORMED STARTER CHIP DETECTOR INSPECTION IAW AMM 80-11-01-206-014-H00 REV. 127, RESULTS CHECK NORMAL FOR ENG SN: 707425.</P>)

Part: FILTER — NOT REPORTED (STARTER VALVE) · airframe 101,584 hrs · 19,500 cycles

STARTER VALVE PNEUMATIC FILTER - CLEAN AND RE-INSTALL. REPLACED THE STARTER VALVE PNEUMATIC FILTER IAW AMM 80-11-04-002-001-400, REV 127, & 80-11-04-402-011-400, REV 127. CONDITION CHECKED NORMAL.

Part: STRINGER — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND M/D STRINGER CORRODED, BS 1406, S19R. REPAIRED CORROSION AREA IAW EI T2019A53M-2939 REV 1. CONDITION CHECKED NORMAL.

Part: SUPPORT CHANNEL — CORRODED (BS 1415-1540) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT, STATION 1415 TO STA 1540, RBL 12.8.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG 146T5002 SH 1 REV E. JOB COMPLETED AND CONDITION CHECK NORMAL.&NBSP;</P>)

Part: GUIDE — NOT REPORTED (NR 1 NACELLE) · airframe 101,584 hrs · 19,500 cycles

DAMAGE GUIDE PIN #1 PYLON R/H FAN COWL SUPPORT BEAM HINGE AT FIRST AND THIRD POSITION TOTAL 2EA(<P>REPLACED 1R FAN COWL SUUPORT BEAM FIRST AND THIRD HINGE PIN WITH NEW. IAW&NBSP;<SPAN>AMM 71-11-04-712-011 &AMP;&NBSP;</SPAN><SPAN>AMM 71-11-04-712-012</SPAN></P>)

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 101,584 hrs · 19,500 cycles

CRACK-SKIN, OSS 646.35, RH WING NO. 9 SLAT, UPPER SURFACE(<P>REPAIRED THE CRACK AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV 110. JOB COMPLETED AND&NBSP;CONDITION CHECKS NORMAL.</P>)

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FWD BS 1197 + 66, STRINGER 18L FRAME CORRODED. REPAIRED THE FRAME IAW EI T2019A53M-2779, REV 1. CONDITION CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (OUTFLOW VALVE) · airframe 101,584 hrs · 19,500 cycles

FWD OUTFLOW VALVE CANT FULLY CLOSE DURING PFM CABIN PRESSURING TEST(<P>REPLACE THE OUTFLOW VLV ACTUATOR. PERFORM CABIN PRESS TEST AND RESULT PASS IAW&NBSP;<SPAN>AMM 21-31-04-004-001&NBSP;&NBSP;</SPAN><SPAN>AMM 21-31-04-404-010</SPAN></P>)

Part: WARNING LIGHT — FALSE ACTIVATION (IDG) · airframe 101,584 hrs · 19,500 cycles

IDG QAD COUPLING-CHECK TORQUE AND CONDITION. PERFORM QAD COUPLING TORQUE CHECK. RESULT NORMAL.

Part: BLOCK — CORRODED (BS 547) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND GROUND BLOCK OF GD00202 LOCATED AT STA 547, WL 123, LBL 55 FOUND CORRODED. REMOVED CORRODED GROUND BLOCK IAW SRM 51-04-02-0G-0 REV 110. INSTALLED NEW GROUND BLOCK ON REPAIR ANGLE IAW EI T2019A53M-2632 REV.2. REMOVED & RE-INSTALLED GD00202 GROUND MODULE PINS PER SWPM 20-90-11 REV 71, WDM 25-53-15 AND 25-53-16 REV. 55, PERFORMED LATERAL GUIDE OPERATIONAL TEST IAW AMM 25-53-00-700-830-010 REV.127 AND THE RESULT WAS SATISFACTORY.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE STARTER) · airframe 101,584 hrs · 19,500 cycles

STARTER CHIP DETECTOR - PERFORM A VISUAL INSPECTION. PERFORM ENGINE STARTER CHIP INSPECTION. RESULT: COND CHK SATIS.</P>)

Part: FILTER — NOT REPORTED (PNEUMATIC SYS) · airframe 10,584 hrs · 19,500 cycles

REPLACE PNEUMATIC HP CONTROLLER AIR FILTER. REPLACED PNEUMATIC HP CONTROLLER AIR FILTER IAW AMM 36-11-08-004-028-007 & AMM 36-11-08-004-032-007. CONDITION CHECKS NORMAL.

Part: COUPLING — LOOSE (PNEUMATIC DUCT) · airframe 101,584 hrs · 19,500 cycles

FOUND ENG (SN: 707425) PNEUMATIC DUCT COUPLING LOOSE AND WITH NO SAFETY WIRE. TOTAL OF 3 LOCATIONS, NEAR FUEL MANIFOLD.(<P>REMOVED ENG (SN 707425) 14TH PNEUMATIC DUCT IAW AMM 70-52-00-912-001 REV. 127. PERFORMED ENG 14TH PNEUMATIC REPAIR AND TEST COMPLETED IAW J/C ATTACHING SHEET 0170761. INSTALLED 14TH PNEUMATIC DUCT IAW AMM 70-52-00-912-001 REV. 127. SUPPLIED PNEUMATIC POWER FOR DUCK LEAK CHECK, NO LEAK FOUND IAW AMM 36-00-00-862-047.</P>)

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 101,584 hrs · 19,500 cycles

NR 3 SLAT, INBOARD NOSE SKIN RIVET SURROUND SKIN MINOR CRACK DAMAGE OSS 723.(<P>REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REV 110. CONDITION CHECK NORMAL.

Part: SUPPORT PLATE — CORRODED (RT AILERON HINGE) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION DAMAGE ON RT WING INBD AILERON HINGE SUPPORT PLATE AT WS 508.(<P>REMOVED CORROSION SUPPORT PLATE IAW SRM 51-40-02-0G-0 REV 110. PERFORMED CORROSION AREA REPAIR IAW EI NO T2019A57M-3398 REV.1. INSTALLED SUPPORT PLATE IAW SRM 51-40-02-0G-0 REV.110 AND BOEING DWG NO 113T1553 SH 1 REV.B. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: FILTER — NOT REPORTED · airframe 101,584 hrs · 19,500 cycles

REPLACE PNEUMATIC PRESSURE CONTROLLER AIR FILTER. REPLACED PRVC AIR FILTER IAW AMM 36-11-19-004-027-002, REV 127, AND AMM 36-11-09-402-114-001 REV 127. CONDITION CHECKED NORMAL.

Part: STRINGER — CORRODED (BS 544-566) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND STRINGER S-32L, STA 544 - 566 CORRODED. REPAIRED AREA IAW EI T2019A53M-2632, REV 2. CONDITION CHECKED NORMAL.

Part: PLUG — LEAKING (THRUST REVERSER) · airframe 101,584 hrs · 19,500 cycles

FOUND #2 ENG R/H T/R ACTUATOR UP PLUG LEAK.(<P>REPLACED #2 T/R OPEN ACTUATOR UPPER HOSE PLUG WITH SERVICEABLE PARTS 20-11-00-910-801. OPEN AND CLOSE THE T/R. CHECK NORMAL AND NO LEAK FOUND.</P>)

Part: SUPPORT ANGLE — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

CORROSION - SUPPORT ANGLE, AFT CGO COMPARTMENT, STA 1329 TO STA 1335, RBL 14.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV. 110. FABRICATED NEW STRAP IAW EI NO T2019P53M-2875 REV. 0. INSTALLED NEW STRAP IAW SRM 51-40-02-0G-0 REV 110, DWG NO 146T5000 SH18 REV G, AND DWG NO 452T2002 SH6 REV.A. JOB COMPLETED AND&NBSP;CONDITION CHECKS NORMAL.</P>)

Part: ANGLE — BROKEN (AFT CARGO DOOR) · airframe 101,584 hrs · 19,500 cycles

BROKEN - ANGLE, AFT CGO DOOR ANGLE INNER LOWER SIDE.(<P>REPAIRED DAMAGE AREA IAW EI NO T2019A52M-2884 REV 1. JOB COMPLETED AND&NBSP;CONDITION CHECKS NORMAL.</P>)

Part: MODULE — CORRODED (BS 590) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

FOUND GROUND MODULE GD04170B LOCATED AT BS 590, WL127, LBL 60 CORRODED. REMOVED CORRODED GROUND MODULE IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW GROUND MODULE IAW SRM 51-40-02-0G-0 REV.110. REMOVED & REINSTALLED GD04170B GROUND MODULE PINS IAW SWPM 20-90-11 REV. 71, WDM 25-53-17 AND 25-53-15 REV. 55, PERFORMED A LATERAL GUIDE OPERATIONAL TEST IAW AMM 25-53-832-010, RESULT WAS SATISFACTORY.

Part: BRACKET — CORRODED (BS 1263) · corrosion level 2 · airframe 101,584 hrs · 19,500 cycles

BRACKET, AFT CGO COMPARTMENT AT STA 1263, BETWEEN LBL 6.5 AND LBL 22.5 CORRODED. REPLACED THE BRACKET WITH NEW IAW SRM 51-42-01-0G-0 REV.110, DWG 453T1227, SH 2, REV A, AND 453T1223 SH 3.