N393UP

Part: GEARBOX — STUCK (SLAT SYS) · airframe 91,278 hrs · 21,645 cycles

WHILE EXTENDING FLAPS FROM UP TO 1, RECEIVED LE FLAP ASYM EICAS MSG AND LEADINGEDGE DISCRETE LIGHT. INSTALLED INBOARD AND OUTBOARD ROTARY ACTUATORS AND OFFSET GEARBOX IAW. AMM 27-81-20 PB 201 REV. 146. AFTER INSTALLATION OF LEADING EDGE SLAT #8, #9 AND #10 AND INCLUDED ADJUSTMENT IAW. AMM 27-81-02 PB 201 AND PB 501 REV. 146 PERFORMED OPERATIONAL CHECK OF LE SLAT AND FLAP SYSTEM IAW. AMM 27-81-02-715-073 REV. 146. FOUND ALL SATIS.

Part: KNOB — OUT OF ADJUST (DISPLAY) · airframe 90,706 hrs · 21,277 cycles

CREW REPORTS THAT THE TILT KNOB POSITION DID NOT MATCH WITH THE INDICATION ON THE NAV DISPLAY. TILT KNOB ADJUSTED IAW AMM 34-43-02 PB401 REV.144. AND TESTED IAW AMM 34-43-00 PB501 REV.144. FOUND SATIS.

Part: IDG — FAILED (ZONE 400) · airframe 90,504 hrs · 21,131 cycles

ATB L GEN OFF DURING TAKEOFF ROLL. RAN CHECKLIST, RESULTED IN MOMENTARY GEN OPERATION BEFORE FAILING AGAIN. ATB REPLACED JAW AMM 24-22-02 PB 401 SATIS

Part: DRAIN — NONE · airframe 90,252 hrs · 20,950 cycles

FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPEN

Part: NONE — NONE (NONE) · airframe 90,254 hrs · 20,951 cycles

FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 90,252 hrs · 20,950 cycles

MAJOR REPAIR, DAMAGE - FOUND M/D FLOOR PNL DAMAGE P/N:371-53-15-C6405-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-15-C6405-101.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 90,252 hrs · 20,950 cycles

MAJOR REPAIR, DAMAGE , FOUND M/D FLOOR PNL DAMAGE P/N: 368-53-00-95626-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-00-95626-101

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 90,252 hrs · 20,950 cycles

MAJOR REPAIR, DAMAGE FOUND M/D FLOOR PNL DAMAGE P/N:371-53-13-C4218-103 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-13-C4218-103

Part: HANDLE — BROKEN (ZONE 800) · airframe 90,254 hrs · 20,951 cycles

FOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE 1. I.A.W AIPC 52-11-25-13-144 REV.28 TO REMOVE FWD ENTRY DOOR HANDLE. 2. I.A.W AIPC 52-11-25-13-144 REV.28 TO INSTALL NEW FWD ENTRY DOOR HANDLE. 3. I.A.W AMM TASK 52-11-00-715-128 REV.143 TO DO OPERATIONAL TEST. THE RESULT WAS SATISFIED. 4. PARTS INFORMATION ATTACHED. 5. IPC VERIFIED AND SERVICEABLE PARTS TAG NO. 038118. 6. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 90,252 hrs · 20,950 cycles

CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE)

Part: PUMP — CRACKED (ZONE 500) · airframe 90,254 hrs · 20,951 cycles

*** SUPPLEMENTAL SDR *** FAULT - CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV 143 REPLACE THE R/H WING AUX FUEL PUMP PNLNO.631AB. 2.CONDITION CHECK NORMAL. 3.IPC VERIFIED AND SERVICEABLE TAG NO.:676139 4.ATTACHMENT ARE UPLOADED

Part: BEARING — BROKEN (ZONE 800) · airframe 90,252 hrs · 20,950 cycles

FOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE OK TO WORK

Part: SKIN — DENTED (ZONE 100) · airframe 90,252 hrs · 20,950 cycles

DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORK

Part: SKIN — DENTED (APU DOOR) · airframe 90,252 hrs · 20,950 cycles

DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) OK TO WORK

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 90,254 hrs · 20,951 cycles

CRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR) INSTALLED LEFT WING NO.3 SLAT CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.126

Part: SKIN — CRACKED (ZONE 500 LE) · airframe 90,254 hrs · 20,951 cycles

*** SUPPLEMENTAL SDR *** FAULT - CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR) INSTALLED L/H WING LEADING EDGE UPPER FIX PANEL I.A.W SRM 51-40-02-0G REV.126 AND BOEING DWG 114T2230 SH1 REV.D AND 114T2510 SH1 REV.E AND 114T2120 SH1 REV.G AND 114T2800 SH2 REV.C

Part: SKIN — DENTED (ZONE 100) · airframe 90,295 hrs · 20,964 cycles

DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-36R (EVALUATE) MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.6" DEPTH(Y)=0.007" AND A/Y = 85 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126

Part: SKIN — DENTED (ZONE 500) · airframe 90,252 hrs · 20,950 cycles

CRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR)

Part: SKIN — DENTED (ZONE 500) · airframe 90,252 hrs · 20,950 cycles

CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR)

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 90,252 hrs · 20,950 cycles

MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1197+132~1329, LBL11~RBL11, P/N:368-53-16-94477-127 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-94477-127.

Part: SKIN — DENTED (ZONE 100) · airframe 90,252 hrs · 20,950 cycles

DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORK

Part: SKIN — DENTED (FUSELAGE) · airframe 90,295 hrs · 20,964 cycles

SKIN DENTED, RT FUSELAGE TAIL SECTION BS 1915.1 - 1923.5. MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.4" DEPTH(Y)=0.006" AND A/Y = 66 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126

Part: SKIN — DENTED (APU DOOR) · airframe 90,254 hrs · 20,951 cycles

*** SUPPLEMENTAL SDR *** FAULT - DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) 1. MEASURED THE DENT DIMENSION LENGTH=0.8" WIDTH(A)=0.5" DEPTH(Y)=0.005" AND A/Y = 100 FOUND TO BE IN LIMIT PER SRM 52-40-01-1A-6 FIGURE 101 DETAIL IV REV.126 2. SUBMITTED DETAILS TO ADM FOR TRACKING AND VISIBILITY DEFERRED AS INFO-CLASS DEFERRAL. 3. JOB COMPLETED.

Part: SKIN — DENTED (ZONE 100) · airframe 90,252 hrs · 20,950 cycles

DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORK

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 90,252 hrs · 20,950 cycles

MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1121.1~1197, LBL 11 ~ RBL 11, P/N:368-53-16-94477-109 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-94477-109.

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 90,254 hrs · 20,951 cycles

CRACK - SKIN, LOWER FACE OF L/H WING NO.6 SLAT MID LINK LOWER DOOR (REPAIR) 1.I.A.W AMM 57-41-59-404-009 REV 143 INSTALLED THE LEFT WING NO.6 SLAT MIDDLE LINK DOOR, AND PERFORMED THE DOOR ADJUSTMENT WAS SATISFIED. 2.CONDITION CHECK NORMAL.

Part: A/C PACK — ODOR · airframe 90,019 hrs · 20,769 cycles

STRONG ACRID OIL SMELL WITH PACKS ON WHILE USING BLEED AIR FROM APU ALSO NOTICED FILM ON INSIDE OF WINDOW AND CAUSED EYE IRRITATION AFTER LONG APU RUN WITH BOTH PACKS ON, THE SMOKE SMELL DISAPPEARED. OPS TEST PERFROMED IAW AMM 21-00-21-102-030, REV: 142.

Part: VALVE — WARNING MESSAGE (ENGINE) · airframe 89,882 hrs · 20,659 cycles

*DIVERSION* R ENG PRV STATUS MESSAGE ON TAKEOFF #2 ENG PRV MANUAL WRENCHING ACCOMPLISHED AND VERIFIED TO BE HARD TO WRENCH AND WITH STUCK POSITION IN THE MIDDLE. THEREFORE #2 ENG PRV REPLACED AS PER AMM 36-11-18/401 REV.141 OPS AND LEAK TEST FOUND SATIS.

Part: ADC — FAULTED (UNKNOWN) · airframe 89,519 hrs · 20,404 cycles

ATB, IN FLIGHT ALT DISAGREE? EICAS MESSAGE DISPLAYED. 1ST OFFICER AIR DATA DETERMINED TO BE AT FAULT, ALT AIR DATA SELECTED PERFORMED T/S ON PITOT & STATIC SYS AS PREVIOUS TESTS SHOWED AN ALTITUDE DIFFRENCE OF 100 FEET BETWEEN CAPT AND F/O SIDE. CHECKED ALL CONNECTIONS OF ALL PITOT - STATIC DEVICES DOWN TO ADCS. NO FAULTS OR LEAKS NOTED. TO ISOLATE TOO MANY POSSIBLE FAULTS SOURCES, INSTALLED TEST SET UP ON CPT & F/O SIDE SEPERATELY. PERFORMED TEST IAW AMM: 34-11-00-862-045, REV: 140. DIFFERENCE BETWEEN CPT AND F/O IS AT MAXIMUM TO THE TESTSET IS MAX 30 FT AND DIFFRENCE OF CAPTAIN TO F/O SIDE IS MAX 20 FT. LEAK TEST OF SYSTEM SATIS & OPS TEST OF FLIGHT DECK ALTITUDE INDICATION WITHIN LIMITS. A/C OK FOR SERVICE.

Part: NONE — NONE (POWERPLANT) · airframe 87,465 hrs · 18,998 cycles

INSPECTION TYPE:N/A**ATB ** - L ENG FUEL FILT AMBER MSG APPEARED DURING CLIMB. AMBER MSG DISAPPEARED AND RETURNED BRIEFLY AT MAX CRUISE THRUST. L ENG FUEL FILT WHITE STATUS MESSAGE APPEARED AND REMAINED FOR REMAINDER OF FLIGHT. THE AMBER EICAS MESSAGE RETURNED BREIFLYREMOVED AND REPLACED LEFT ENGINE FUEL FILTER ELEMENT PER M/M 73-11-02 SECTION 3 THIS PAGE FOR TEST [ MB 0557925 10/15/21] REPLACED FUEL FILTER DIFERRENTIAL PRESSURE SWITCH REF AMM 73-34-01. OPS CHECK LEAK CHECK GOOD. PERFORMED TEST OF L/H ENG FUEL FILTER REF AMM 71-00-00-995-229-H03

Part: NONE — POPPED (POWERPLANT) · airframe 87,459 hrs · 18,994 cycles

INSPECTION TYPE:N/A*ATB* NO EMERG DECL'D* A/C LANDED WITHOUT INCIDENT* RIGHT FUEL PRESSURE CB POPPER @ 12000 DURING OLIMLOST RETURN TO SDFREPLACED CANNON PLUG NO. D10998 REF WDM 73-33-11. COMPLIED WITH 10 MIN ENG RUN AMM 71-00-00. OPERATIONAL CHECK NORMAL ESR WDM 73-33-11