N393UP
Registered owner: CARGO AIRCRAFT MANAGEMENT INC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
MAIN ENTRY DOOR LATCH UNABLE TO LOCK. PERFORMED OPERATIONAL TEST OF CREW ENTRY DOOR REF AMM 52-11-00. OPS CHECKED GOOD. DOOR CLOSES AND LOCKS AS INTENDED
MAJOR REPAIR, OVERSIZE RIVET HOLES, IN SLAT INSERT FITTING AND SLAT LEADING EDGE RIB ATTACH FASTENERS NR 9 SLAT ALL STEPS OF EO-96917-REQ7 C/W.
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.
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.
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
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPEN
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR
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
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
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.
CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE)
FOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE OK TO WORK
*** 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
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.
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.
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.
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
DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORK
CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR)
CRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR)
DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) OK TO WORK
DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORK
DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORK
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
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
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.
*** 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.
*** 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
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.
*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.
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.
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
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