N612FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORP | Operator | 2010-03-23 – 2010-03-23 | Operator named in NTSB report |
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | 2010-03-23 – 2010-03-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SLAT DISAG. SLATS DID NOT EXTEND. LANDED SLATS UP WITH FLAPS 28. EMERGENCY DECLARED. PERFORMED FIM 27-80-00-1, FOUND ALL SLATS TO BE OPERATING NORMALLY. PERFORMED FIM 31-71-07-00 FOR SLAT DISAG ALERT. AT PSEU, SENSOR LIGHT SHOWN FOR CHANNEL 32, INDICATING PROXIMITY SWITCH FAILURE OF RT NR 2 SLAT B SENSOR. REPLACED SENSOR IAW AMM 27-84-02-4. OPS CHECK GOOD, SLATS OPERATE NORMALLY AND INDICATE NORMALLY. OKAY FOR SERVICE.
DURING CRUISE WE RECEIVED A LEVEL 1 HYD 1 OFF ALERT. COMPLIED WITH QRH. HYD 1 QUANTITY WAS 3.0 GALLONS. DECLARED AN EMERGENCY WITH MEMPHIS APPROACH IN ANTICIPATION OF A LEVEL 2 HYD 1 FAIL ALERT. COMPLIED WITH QRH AND PERFORMED AN APPROACH AND LANDING TO KMEM 36C. RECEIVED THE LEVEL 2 HYD 1 FAIL ALERT DURING LANDING ROLL. EXITED THE RUNWAY, SET THE PARKING BRAKE, STARTED THE APU, AND SHUTDOWN ALL 3 ENGINES. ***EMERGENCY DECLARED*** #1 EDP'S WERE NOT RAN DRY 1.6 GALLONS REMAINS IN SYSTEM 1, IN CENTER WHEEL WELL 1-3 RMP INLET LINE TO #1 S/O VALVE HAS A STATIC LEAK, POSSIBLE O RING RUPTURE. MORE T/S AND CLEANUP REQUIRED FOUND THE O RING FOR THE INLET FOR THE 1-3 RMP DAMAGED AND LEAKING. REMOVED AND RELACED INLET O-RING , ITEM 340 IN IPC 29-22-01-01, IAW AMM 29-22-20-2. OPS AND LEAK CHECKS ARE GOOD AT THIS TIME. ORIG SUB DATE: 10/3/2022
ENROUTE RECEIVED LEVEL 1 HYD 3 ELEV. OFF, THEN HYD 3 OFF, LEVEL 2 HYD 3 FAIL AND QTY WENT TO 0.1. DECLARED EMERGENCY, DUMPED 77.0 LBS OF FUEL AND DIVERTED TO RJBB. T/SHOT AND FOUND #3 ENG L/H EDP CASE DRAIN RIGID LINE HAS CRACK/HOLES CAUSED BY CLAMP BROKEN. REF AIPC 29-11-15-01ITEM# 70. P/N 224-9409-529 CASE DRAIN RIGID LINE REPLACED REF. WRI 71-10/1824 R&R'ED #3 ENG L/H EDP W/ RIGID CASE DRAIN LINE PER AMM 29- 11-20-4-1. R&R'ED ALL CASE DRAIN FILTERS PER AMM 29-12-41-2.
LEFT LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. EMERGENCY DECLARED. RETURNED TO AUS. REMOVED MLG UNLOCK CYLINDER AND INSTALLED LH MLG UNLOCK CYLINDER. LEAK CHECK IS GOOD. REF. AMM 32-33-02-4. INSTALLED NEW CLAMPUP BUSHING. COMPLETED INSTALLATION OF L MLG UNLOCK CYLINDER. LEAK CHECK GOOD. AMM: 32-33-02-4.
FUSELAGE LEFT HAND SIDE , SKIN FORWARD OF MAIN CARGO DECK CARGO DOOR FORWARD JAMB AT APPROXIMATELY STA 604.75 LONGERON 24 LEFT AREA HAS A SMALL DENT. EA # 1-5300-T0357118A P4 REQUIRES A PERMANENT REPAIR TO BE CARRIED OUT. FUSELAGE LEFT HAND SIDE , SKIN FORWARD OF MAIN CARGO DECK CARGO DOOR FORWARD JAMB AT APPROXIMATELY STATION 604.75 LONGERON 24 LEFT DENT AREA REPAIRED AS PER E.A. # : 1-5300-T0357118 B PART 4. TITLE: FUSELAGE - DENT REPAIR ON FUSELAGE SKIN FORWARD OF MAIN DECK CARGO DOOR JAMB , STATION 604 , L -24L. REFER TO WRI: 53000548 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100..
DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON ALL AFFECTED / ACCESSED FASTENER HOLES AT LEFT HAND NOSE LANDING GEAR TRUNNION IN ACCORDANCE WITH EA 1-5310-T0362355 P1 STEP 2, FOUND CRACK INDICATION ON FASTENER HOLE AT STATION 583 LONGERON 49 LEFT. LEFT HAND NOSE LANDING GEAR STATION 583 LONGERON 49 LEFT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FABRICATED LONGERON AS PER DOUGLAS DRAWING ACA3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK APPROXIMATE 0.1" EXTENDED FROM EXISTING STOP DRILL HOLE ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AT STATION 595. LEFT HAND NOSE LANDING GEAR STATION 595 TRUNNION FITTING REPAIRED AS PER EA 1-5310-T0362355 P1 TITLE : FUSELAGE - MAINFRAME - CRACK REPAIR ON LH NOSE LANDING GEAR TRUNNION FITTING, STA 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
02 EACH FASTENER HOLES #6 AND #11 FOUND CRACK INDICATION DURING OPEN - HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6. 02 EACH FASTENER HOLES #6 AND #11 WITH CRACK INDICATION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 BUSHING REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC INSPECTION PER SRM 57-20-02-2R FIGURE 202 / REPAIR 5 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING OUTER REAR SPAR LOWER CAP CRACKED BETWEEN STATION XORS 1043 - 1045. CRACKED AREA AT LEFT HAND WING OUTER REAR SPAR LOWER CAP BETWEEN STATION XORS 1043 - 1045 REPAIRED AS PER SRM 57-20-10-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO - RIGHT HAND TUNNEL STATION 5-113 TO STATION 1541 LONGERON 35 RIGHT LONGERON SPLICE FOUND CRACKED. CENTER CARGO RIGHT HAND TUNNEL STATION 5-113 TO STATION 1541 LONGERON 35 RIGHT CRACKED LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A7114 REVISION : J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO - STATION 5-113 TO STATION 1541 LONGERON 44 RIGHT LONGERON SPLICE FOUND CRACKED. CENTER CARGO STATION 5-113 TO STATION 1541 LONGERON 44 RIGHT CRACKED LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A7114 REVISION : J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 756 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 756 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 634 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 634 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 705 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 705 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 765 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 765 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING LEADING EDGE COMPARTMENT FORMER FOUND CRACKED AT STATION XOS 939. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB1292 REVISION G. INSTALLED FABRICATED FORMER AT RIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 939 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING LEADING EDGE # 11 SLAT TRACK CUTOUT FOUND CRACKED AT STATION XOS 719. RIGHT HAND WING LEADING EDGE # 11 SLAT TRACK CUTOUT AT STATION XOS 719 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 791 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 791 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 649 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 649 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 649 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 649 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 553 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 553 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 543 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 543 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 650 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 650 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
SMIS 612 57-20 0638 22MAY21 MEM FACT U MOD TYPE T MOD NO. 1-5720-T0361818 REV NO. PS P1 WING -OUTER WING- LEFT WING SPAR LOWER CAP CRACKED BETWEEN XORS=1043-1045: PREP COMPLY WITH E..A. 1-5720-T0361818 REV NO. POS. P1 INFO 23MAY21 00:30 ** ATTACHED TO WORK ORDER 00080239 ** FACT 23MAY21 01:16 IND U COMPLIED WITH EA 1-5720-T0361818 P1 FOR PREPARATION OF MX FERRY INFO 23MAY21 00:30 ** ATTACHED TO WORK ORDER 00080239 ** FACT 23MAY21 01:16 IND U COMPLIED WITH EA 1-5720-T0361818 P1 FOR PREPARATION OF MX FERRY
MDIS 612 57-30 0764 26MAY21 IND OPEN U L/H WING LOWER SPAR CAP CRACKED BETWEEN STATION XORS1043-1045 CRACKED AREA AT L/H WING OUTER REAR SPAR LOWER SPAR CAP BETWEEN STATION XORS1043- 1045 HAS BEEN REPAIRED AS PER SRM 57-20-10-2R FIG 201 REPAIR 1.
ON TAKEOFF PASSING 3000 FT, MOMENTARY LEVEL 3 MANF 3 FAIL ALERT FOR ABOUT 3 SECONDS ALERT WENT AWAY AND #2 BLEED VALVE CLOSED. REF WDM 36-23-02 PG 1 SH 1, REMOVED MFC REF AMM 36-23-01-4. CONTINUITY CHECKED GOOD AT R5-1054A BETWEEN PINS 5C AND 6C. FROM ANY OF THOSE PINS, FOUND A 1.5K OHMS SHORT TO GROUND. ISOLATED D1-125 AND SHORT WENT AWAY. REPLACED D1-125 REF AMM 36-23-07-4. INSTALLED MFC REF AMM 36-23-01-4. ALL TEST PASS.
DURING WALKAROUND , FOUND BULK CARGO DOOR BENT . MAJOR SHEETMETAL REPAIR PERFORMED PER EA 1-5200-T0354075
LEFT HAND WING LEADING EDGE CAVITY ÿ½ UPON REMOVAL DOUBLER AT XOS 667, STRINGER FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE CAVITY ÿ½ UPON REMOVAL DOUBLER AT XOS 667, STRINGER AS PER SRM 57-40-03-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT STATION BETWEEN 5 ÿ½ 53 TO 5 ÿ½ 73 RIGHT HAND LONGERON SPLICE 48 FOUND CORRODED. CENTER CARGO COMPARTMENT STATION BETWEEN 5 ÿ½ 53 TO 5 ÿ½ 73 RIGHT HAND LONGERON 48 SPLICE CORRODED, FOUND EXFOLIATED AND OUT OF LIMIT PER SRM 53-00-00-2R FIGURE 202. SPLICE REMOVED AS PER SRM 51-31-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AEA7653 REVISION B, PART NUMBER AEA7653-1 AND INSTALLED AS PER MD11 SRM 51-31-01-0G AT CENTER CARGO COMPARTMENT STATION BETWEEN 5-53 TO 5-73 LONGERON 48 RIGHT HAND. REPAIR CLASSIFIED AS MAJOR PER 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT RIGHT HAND STATION 1522, X = - 107.25. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT RIGHT HAND STATION 1522 X= -107.25 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1491 TO EXISTING SPLICE AT STATION 1531 X = - 107.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING LEADING EDGE CAVITY DOUBLER AT XOS 667 FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT RIGHT HAND STATION 6 - 02, X = - 8.5. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT RIGHT HAND STATION 6-02 X=-8.5 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 6-40 TO EXISTING SPLICE STATION 6-0 X = - 8.5 AS PER SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT LEFT HAND STATION 1371, X = 75.25. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT LEFT HAND STATION 1371 X= 75.25 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1266 TO STATION 1391 X = 75.25 AS PER SRM 53- 00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK STATION 1851 LEFT HAND X = 8.5 SEAT TRACK FOUND CORRODED. MAIN DECK STATION 1851 LEFT HAND X = 8.5 SEAT TRACK CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1831 TO STATION 1887 END X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM NO. N01045 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT RIGHT HAND STATION 1134, X = - 8.5. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT RIGHT HAND STATION 1134 X=-8.5 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1129 TO STATION 1189 X = - 8.5 AS PER SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT RIGHT HAND STATION 1239 ÿ½ STATION 1256, X=-8.5. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT STATION 1239 ÿ½ STATION 1256, X=-8.5 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1266 TO EXISTING SPLICE AT STATION 1229 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND LEADING EDGE CAVITY DOUBLER AT XOS 667 FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK STATION 1841 TO 1851 LEFT HAND X = 8.5 SEAT TRACK FOUND CORRODED. MAIN DECK STATION 1841 TO 1851 LEFT HAND X = 8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1831 TO STATION 1887 END X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
HFEC INSPECTION CARRIED OUT ON NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING EXISTING TRIMMED OUT AREA CRACK GROWTH APPROXIMATE 0.25 INCHES AT STATION 595 . NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING EXISTING TRIMMED OUT AREA CRACK GROWTH APPROXIMATE 0.25 INCHES AT STATION 595, CARRIED OUT REPAIR AS PER SRM 53-10- 14-2R FIGURE 202, REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1,500 FLIGHT CYCLES AFTER REPAIR AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 1,500 FLIGHT CYCLES AS PER SRM 53-10-14 TABLE 201, FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FUSELAGE: CENTER LANDING GEAR WHEEL WELL LEFT HAND BULKHEAD APPROXIMATE STATION 1381, FEED THRU DOUBLER FOUND CRACKED. CENTER LANDING GEAR WHEEL WELL LEFT HAND BULKHEAD APPROXIMATE STATION 1381, CRACKED DOUBLER REMOVED AND INSTALLED WITH FABRICATED DOUBLER AS PER SRM 51- 33-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
02 EA CRACK INDICATION FOUND APPROXIMATELY 0.3ÿ½ & 0.1ÿ½ IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SLAT DOOR INBOARD CORNER ( CORNER #5) AT XOS 490. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE SLAT DOOR INBOARD CORNER (CORNER #5) AT XOS 490 AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
01 EA CRACK INDICATION FOUND APPROXIMATELY 0.1ÿ½ IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SLAT TRACK #10 INBOARD CUTOUT ( CORNER #13) AT XOS 657. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE SLAT TRACK #10 INBOARD CUTOUT (CORNER #13) AT XOS 657 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING LEADING EDGE CAVITY FORMER AT XOS 993 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB1164 REVISION M. INSTALLED FABRICATED FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT XOS 993 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING LEADING EDGE CAVITY AT STATION XOS 789 DOUBLER CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE CAVITY AT STATION XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING LEADING EDGE CAVITY AT STATION XOS 667 DOUBLER CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT HAND WING LEADING EDGE CAVITY AT STATION XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING LEADING EDGE CAVITY AT XOS 667 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 667 BEADED DOUBLER AREA AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
PDIS 612 29-10 9067 31JAN20 PHX OPEN U LOGPAGES:3163545 RECEIVED HYD 1 OFF LEVEL 1 ALERT DURING CRUISE FLIGHT DUE TO DECREASING FLUID QTY IN SYSTEM 1 COMPLIED WITH QRH SHGN 31JAN20 02:29 PHX U #1 HYD QTY AT A/C BLOCK IN WAS 2.2 & PER CREW DEBRIEF DID NOT GO BELOW 1.9 DURING FLIGHT. FACT 31JAN20 12:22 PHX R&R'D RIGHT EDP (LOWER) IAW AMM: 29-11-20-4-1. OPS CHECK GOOD. A/C OK FOR SERVICE.
ON DEPARTURE, THE FIRST WAY POINT " NEZUG" SEQUENCED TO THE "FROM" (IL) BUT THE FD COMMANDED A RIGHT TURN TO THE 071 DEG HEADING, 7 MILES EARLY. DEPARTURE THEN VECTORED US BACK ON COURSE AND STOPPED OUR CLIMB. TCAS ALERT FOLLOWED BRIEFLY. FSR WILL BE FILED. RAN RTS ON IRU'S PER 34-43-00-5-0, RAN RTS ON DEU'S PER 31-61-02-5-0, RAN RTS ON FMC'S 34-63-00-5-0, ALL TESTS PASSED. PERFORMED AUTOFLIGHT AND AUTO LAND PER AMM 22-00-00-2 OP'S CHECK GOOD. SENSOR STATUS PAGE FMC SHOWED GOOD. FOLLOWED FIM 22-00-00-2. ALL CHECKS GOOD OK FOR CONTINUED SERVICE.
GEAR HANDLE RAISED, 4 RED LIGHTS REMAINED & FELT DRAG ON A/C. CHECK LIST ACCOMPLISHED & GEAR RAISED A 2ND TIME, ALL LTS RED INCLUDING CONFIG PAGE. LANDED 4 GREEN. PERFORMED GEAR SWINGS TO VERIFY OPERATION AND TROUBLE SHOOT. FOUND THE ALTERNATE GEAR LEVER SWITCH TO BE BAD. REMOVED AND REPLACED SWITCH IAW AMM 32-32-01-4. PERFORMED NORMAL AND ALTERNATE GEAR SWINGS IAW AMM 32-31-00-5. ALL OPERATIONS AND INDICATIONS NORMAL. SEE SDR # 19-2214. SWITCH PN H20-24B CPN 0030004.
MDIS 612 25-60 8295 03JUL19 IND OPEN U LOGPAGES:2800327 POST FLIGHT INSPECTION FOUND L1 DOOR EVAC SLIDE PRESSURE, PRESS TO TEST LIGHT INOP. MEL 03JUL19 03:12 IND U RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 13JUL19 "MEL 25-61-02: L 1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." FACT 06JUL19 01:34 EWR REMOVED AND REPLACED BATTERIES IN L1 DOOR SLIDE BOTTLE PRESS PTT PER AMM 25-61-04-4. OPS CK GOOD. REMOVED ITEM FROM MEL.
AFTER TAKEOFF AT VR, TR-3 FAIL LEVEL 1 ALERT, DISPLAYS 4-6 AND MCDU NR 2 WENT BLANK. RAN QRH. AT BLOCK IN WITH EXTERNAL POWER CONNECTED TR3 CAME BACK ON. OPS CHECKED THE R2-18 IAW AMM 24-25-03-2, TR3 OPS NORMAL IAW AMM 24-31-01-2, AND WDM 24-57-07.
LEFT WING STRINGER DOUBLER XOS 900 LEADING EDGE SKIN, FOUND CRACKED FROM FASTENER HOLE TO STRINGER EDGE. REPAIRED IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
VERTICAL STAB ACCESS PANEL 363ML CUTOUT FOUND TWO CRACKS, VSS 2154. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING HFEC INSPECTION, CARRIED OUT AT LOWER VERTICAL STABILIZER REAR SPAR CAP RT FWD FLANGE UPPER SECTION, AND FOUND ONE CRACK 3.70 INCHES LONG, HSS 2164. REPAIRED IAW EA 1-5530-T0339048, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING HFEC INSPECTION, CARRIED OUT AT LOWER VERTICAL STABILIZER REAR SPAR CAP, LT FWD FLANGE UPPER SECTION, FOUND ONE CRACK 1 INCH LONG AT HSS 2164. REPAIRED IAW EA 1-5530-T0339008, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK L3 DOOR FRAME LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L TO 27L FOUND CRACKED. THE L3 DOOR FRAME LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE AT XOS 991.5 LEADING EDGE SKIN FOUND CRACKED ABOUT 8 INCHES. REPAIRED IAW SRM 57-40-01-2R, FIG 261, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE AT XOS 991.5 LOWER SURFACE DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RT EXISTING REPAIR AT MAIN DECK CARGO FLOOR SEAT TRACK STA.625 TO STA.645 X = -47.5 RT EVALUATED AND FOUND CHAFED DAMAGE AT SEAT TRACK CROWN. MAIN DECK CARGO FLOOR SEAT TRACK AT STA.625 TO STA.645 X = -47.5 RT CARRIED OUT REPAIR PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. SEAT TRACK CROWN BLENDED AREA EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
MAIN DECK FLOOR SEAT TRACK AT BS 1406, RBL 47.5. FOUND CROWN DAMAGED. GOUGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 6-80, RBL 47.5 CROWN DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STA 5-6 X= 27.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING A POSTFLIGHT CHECK, FOUND RIGHT SIDE EVACUATION SLIDE, REMOTE PRESSURE PRESS-TO-TEST SWITCH INOPERATIVE. R1 DOOR REMOTE PRESSURE INDICATOR ASSEMBLY REMOVED AND REPLACED, OPS TEST CARRIED OUT IAW AMM 25-61-04-4, AND AMM 25-61-04-710-801. FOUND SATISFACTORY.
HORIZONTAL STAB TRIM RATE 2 CIRCUIT BREAKER FOUND OPEN. CONFIGURED THE ACFT TO OPS CHECK THE STAB TRIM MOTOR IAW MM 27-41-00-5, THE CIRCUIT BREAKER TRIPS DURING OPS CHECK. REMOVED AND REPLACED THE NR 2 HORIZONTAL STAB TRIM MOTOR SOSV IAW AMM 27-43-31-4, ALL TESTS PASSED. OPS CHECKED GOOD.
INFORMED BY ATC SOMETHING FELL OFF OUR ACFT ON TAKE OFF. CONFERED WITH GOC AND MOC AND DECIDED TO RTB. REMOVED AND REPLACED THE RIGHT NR 1 SLAT IAW AMM 27-80-20-000-801, AND PERFORMED AN ADJUSTMENT TEST IAW AMM 27-80-20-820-801. OPS NORMAL, ACFT OK FOR SERVICE.
AFTER TAKEOFF, PLUS 25 MINUTES, CLIMBING THROUGH FL250, THE NR 2 ENGINE FLAMED OUT. THROTTLES WERE SET AT CLIMB POWER WHEN CONFIRMED ENGINE OUT MESSAGE APPEARED ON MCDU SCRATCH PAD. NR 2 ENGINE PARAMETERS, N1 AT 51.4 %, EGT 335, N2 335, N2 AT 79.4%, FUEL FLOW 2550, AND NORMAL OIL PRESSURE, TEMPERATURE, AND QUANTITY. AUTOTHROTTLES WERE ON. THE NR 2 ENGINE WAS WINDMILLED FOR 40 MINUTES AT IDLE N2 OF 26.5% AND N1 OF 26.8%. AFTER WET MOTORING THE ENGINE, DETERMINED FUEL WAS LEAKING FROM FORWARD GASKET ON THE IDG FUEL/OIL HEAT EXCHANGER. WHEN GASKET WAS REMOVED, FOUND A TEAR IN RUBBER PART OF THE GASKET.
AT 110 KTS, ALT & IAS AMBER ALERTS APPEARED ON THE CAPTAIN`S AND FIRST OFFICER`S PFOS. DURING TROUBLESHOOTING IAW FIM 34-11-01-03, AND 34-11-03-03, FOUND THE NR 2 CADC WOULD NOT TEST. REMOVED AND REPLACED THE NR 2 CADC IAW MM 34-16-01-4, 34-10-00-2, 22-00-00-2. SYSTEM OPS NORMAL, ACFT OK FOR SERVICE.
MCD HINGE LUGS NEED REWORK/WORN LUGS/BUSHING REWORKED REF CMM 52-34-04.
MCD DOOR FWD DOOR HINGE LUG/BUSHING WORN LUG/BUSHING REWORKED REF CMM 52-34-04.
LUGS NEED REWORK/WORN LUGS/BUSHING REWORKED REF CMM 52-34-04.
MCD FWD HINGE HAS 8 EACH LUGS NEED REWORK LUGS/BUSHING REWORKED REF CMM 52-34-04.
AIR CONDITIONING DOOR STRUCTURE ON THE PLANE AFT UPPER CORNER APPEARS TO BE CRACKED. REPAIRED THE AREA IAW SRM 53-20-15.
ONE EACH FASTENER HOLE NR 6 FOUND CRACK INDICATION, DURING OPEN HOLE HFEC INSPECTION, AT LT WING LOWERS SKIN ACCESS DOOR CUT OUT, BETWEEN STATION XORS 690 - XORS 700. REPAIRED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2,000 FLIGHT CYCLES & REPETITIVE INSPECTION AT 2,000 FLIGHT CYCLES IAW SRM 57-20-02-2R FIG 202 REPAIR NR 5 TABLE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.255", FINAL HOLE DIAMETER 1.285", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-68411D PT 5 STEPS 1A & 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
AFT ACCESSORY COMPARTMENT, RT SKIN WITH ANCHOR NUT ATTACH, FWD OF STATION 2164, FOUND CORROSION. SKIN REPAIRED PER SRM 53-70-01-2R FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED FOUND EXCEEDED LIMITS IAW CMM 57-52-04. EXISTING HOLE DIAMETER 1.193", FINAL HOLE DIAMETER 1.196, MAXIMUM ALLOWABLE HOLE DIAMETER 1.15". NEW REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0324457 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.190", FINAL HOLE DIAMETER 1.225" & MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-68411D PT 5 STEPS 1A & 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.215", FINAL HOLE DIAMETER 1.250", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-68411D PT 5 STEPS 1A & 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.257", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324461 PT 1 STEPS 1A & 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE, FOUND CORRODED. CORROSION REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.248", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0324461 PT 1 STEPS 1A & 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.216", FINAL HOLE DIAMETER 1.226 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324432 PT 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503669 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709". NEW REPAIR BUSHINGS, TWO EACH, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-TO324432 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503669 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, UPPER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.957", FINAL HOLE DIAMETER 0.961 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.944". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324432 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503669 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.228 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324433 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503671 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.284", FINAL HOLE DIAMETER 1.289 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324433 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503671 FOR WORK DETAILS.
RIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709". NEW SHOULDER BUSHINGS, TWO EACH FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503670 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324433 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503671 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324433 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503671 FOR WORK DETAILS.
RIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SURFACES, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.412", MATERIAL REMOVED 0.002" & MINIMUM ALLOWABLE THICKNESS 0.423". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503670 FOR WORK DETAILS.
RIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503670 FOR WORK DETAILS.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 543. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.220", FINAL HOLE DIAMETER 1.223 & MAX ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 830, X=-8.5 FOUND CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 785 - 907, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 613. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING LE NR 12 SLAT TRACK CUT OUT OTBD AFT CORNER CRACKEDAT STATION XOS 774.8. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING LE NR 12 SLAT TRACK CUT OUT, OTBD AFT CORNER CRACKED AT STATION XOS 774.8. SKIN REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
HFEC INSPECTION CARRIED OUT ON RT WING LE & FOUND ONE EACH CRACK, APPROX 1.5" LENGTH AT THE FWD INBD CORNER OF THE FUEL ACCESS DOOR AT STATION XOS 610.844. REPAIRED IAW SRM 57-40-01-2R FIG 201 REPAIR 18. INITIAL INSPECTION TO BE CARRIED OUT AT NEXT C CHECK NOT EXCEEDING 24 MONTHS & REPETITIVE INSPECTION AT EVERY C CHECK IAW SRM57-40-01-2R FIG 201 REPAIR 18 TABLE 204. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT BS 1179, X= 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 760. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 738. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 689. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 683. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE, INTERNAL BEADED DOUBLER FOUND CRACK AT XOS 695. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 639. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 631. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE COMPARTMENT, SUPPORT RIB FOUND CRACKED, AT XOS 685. R & R WITH NEW FABRICATED SUPPORT RIB IAW SRM 51-31-01-0G. NEW SUPPORT RIB FABRICATED IAW DWG ARB2924 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 618. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 6-0, X= 8.5 FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 6-0 TO 6-100, X=8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 877, X= 8.5 FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 850 TO 907, X=8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT CABIN FLOOR SUPPORT AT BS 1887 - 2007, X -57 FOUND CRACKED. FLOOR SUPPORT REMOVED IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551 REV G & INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK, AFT CABIN FLOOR SUPPORT AT BS 1887 - 2007, X 25 FOUND CORRODED. FLOOR SUPPORT REMOVED IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087 REV M & INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE, INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 739. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE SKIN SUPPORT RIB FOUND CRACKED, AT XOS 753. R & R WITH NEW FABRICATED SUPPORT RIB IAW SRM 51-31-01-0G. NEW SUPPORT RIB FABRICATED IAW DWG ARB2923 REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE, INTERNAL BEADED DOUBLER FOUND CRACKED, AT XOS 760. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE, INTERNAL BEADED DOUBLER FOUND CRACKED, AT XOS 700. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE, INTERNAL BEADED DOUBLER FOUND CRACKED, AT XOS 737. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING LE NR 6 SLAT, EXTERIOR SKIN, LE FOUND WITH DENT AT STATION XOS 862, REF WRI 5750 2307. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 2 & EA 1-5750-T0324464 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
TO COMPLY WITH EA 1-5330-T0313867 A PART 4 FWD INTERMEDIATE FUSELAGE SKIN PANEL ASSEMBLY. INTERIM REPAIR OF IMPACT DAMAGE AT LOWER FWD CARGO DOOR JAMB CUT OUT. ACCOMPLISHED REPAIR IAW SRM 53-00-15-2R FIG 202 REPAIR 8 & EA 1-5330-T0313867B PT 4. INITIAL INSPECTION TO BE CARRIED OUT AT 12,600 FLIGHT CYCLES & REPETITIVE INSPECTION AT EVERY 6,300 FLIGHT CYCLES IAW SRM 53-00-15-2R FIG 202 REPAIR 8 TABLE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53303668 FOR WORK DETAILS.
AFTER USING ENG & WING ANTI-ICE FOR TAKEOFF, TURNED ANTI-ICE OFF PASSING 1000 FT. THE AIR SYNOPTIC PAGE SHOWING RT WING ANTI-ICE VLV CLOSED & AMBER. NO ASSOCIATED EAD ALERTS. R & R RT WING ANTI-ICE VLV IAW AMM 30-11-01-4. OPERATIONS CHECKED NORMAL. ALSO PERFORMED RETURN TO SERVICE ON ESC IAW AMM 21-08-01-5. ALL TEST PASSED, OK FOR SERVICE.
ON LANDING ROLL RECEIVED LEVEL 3 CABIN SMOKE ALERT UPPER DECK. CREW VERBAL REPORTED, IT LOOKED LIKE WAS WORKING THE PORTION OF MDC AFT OF COMPARTMENT TEMP IND ON AIR PAGE. CABIN SMOKE ALERT EXTINGUISHED BY ITSELF AFTER FEW SECONDS. CHECKED INSIDE OF MDC & FELT HIGH HUMIDITY IN THE COMPARTMENT JUST AFTER BLOCK IN. MOISTURE IS DRIED TO REMOVE FROM MDC COMPARTMENT. OPERATIONS TESTED NORMAL MDC SMOKE DETECTION SYS IAW MM26-15-01-5.
25 MINUTES INTO FLIGHT, FL 280 ENGINE ANTI-ICE ON, WING TAIL OFF, LEVEL 3 AIR MANIFOLD 2 FAIL. QRH PROCEDURE FOLLOWED. REMOVED AND REPLACED C5-87 CONNECTOR IAW EA1-3622-T0314946 REV PS P2. PERFORMED TEST OF THE MANIFOLD FAILURE CONTROLLER AND PASSED IAW AMM 36-23-01-5. RAN ALL ENGINES IAW JRH. ALL PNUMATIC SYSTEMS NORMAL AND NO ALERT ILLUMINATED. PNEUMATIC SYSTEM OPS AND MANIFOLD FAIL DETECTION OPS CHECKED OK IAW AMM 36-10-00-2 & 36-23-00-5.
WRI 57-30/0648 UPPER SKIN ON LT INBD AFT FLAP HAS A 1.2 INCH CRACK. REPAIRED LT UPPER SKIN AFT FLAP DAMAGED AREA IAW SRM57-00-01 REPAIR 1, LEVEL 2 REPAIR CAT A & COMPLIED WITH EA1-5750-T0308108 PT 1 DTD 0513 & 14.
RT WING SPAR CAP DAMAGED. REPAIR SPAR CAP IAW EA 1-5710-164879 REV A PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120
LEFT WING INBD FLAP UPPER SURFACE FOUND DENTED AT STATION XIFH 289. REPAIRED IAW SRM 57-00-01 FIGURE 201 REPAIR 1 REVISION 55.
MAIN DECK SEAT TRACK FLANGE BETWEEN BS 1601 - 1641, X=-8.5 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
MAIN DECK BS 1561 LBL 27.5 SEAT TRACK FOUND WITH CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55.
MAIN DECK BS 1566 RBL 75.25 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55.
LEFT WING FIXED LE BEADED DOUBLER AT XOS 665, FOUND CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIGURE 203 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
MAIN DECK SEAT TRACK FLANGE BETWEEN BS 1601 - 1661, X=8.5 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
DURING A REPETITIVE HFEC INSPECTION ON NLG LT TRUNNION FITTING, CRACK WAS FOUND PROPAGATING FROM THE PREVIOUSLY TRIM OUT AREA APPROXIMATELY 0.25 INCH LENGTH. CARRIED OUT STOP DRILL IAW SRM 53-10-14 FIGURE 203 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS=690 & 700, FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55.
LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS=690 & 700 FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55.
INTERMITTENT CABIN SMOKE INDICATION AFTER LANDING. CREW & AMT CHECKED MDC CONFIRMED THERE IS NO SIGN OF SMOKE OR FIRE NOTED. CREW DEBRIEF THAT ONE EACH MDC SMOKE DETECTOR LOCATED MID AFT ZONE TRIGGER THE FAULT. 30 MINUTES AFTER ACFT LANDED THE MDC SMOKE DETECTION BACK TO NORMAL NO SIGN OF ABNORMALITY. ACFT IS SECURED & TOW BACK TO GATE AS NORMAL PRACTICE. NO HISTORY IN 99 DAYS. TROUBLESHOT IAW 26-15-00/101 CONFIG 1. CARGO SMOKE DETECTORS OPS TESTED & ALL PASSED IAW AMM 26-14-01.
UPON GEAR RETRACTION RT MAIN GEAR UNSAFE LIGHT ILLUMINATED, SYNOPTIC CONFIRMED UNSAFE. FOUND TOP FWD HOSE GUIDE ASSEMBLY, OLD STYLE, ON RT MLG FWD CONDUIT SUPPORT SCISSORS BROKEN. INSPECTED CONDUIT & LATCH ASSEMBLY FOR ADDITIONAL DAMAGE, NONE NOTED. R & R HOSE GUIDE ASSEMBLY IAW MM 32-11-40-4. JACKED ACFT IAW MM 07-11-00-2. ACCOMPLISHED RT MLG GEAR ACTUATION CHECK IAW MM 32-33-00-0. ALL CHECKS SATISFACTORY. ACFT OK FOR SERVICE.
R1 DOOR PRESS-TO-TEST LIGHT DIM. R & R SLIDE BATTERIES. SYS OK FOR SERVICE. FINAL CLOSED.
RT ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST SWITCH INOPERATIVE. R & R RT SLIDE RAFT PRESS TO TEST SWITCH ON REMOTE PRESSURE INDICATER IAW AMM 25-61-04-4, INDICATOR CHECKED GOOD IAW AMM 25-61-04-5.
LEFT EVACUATION SLIDE, REMOTE PUSH TO TEST INDICATOR INOPERATIVE.
DURING PREFLIGHT FOUND SEVERAL BREAKERS POPPED. NR 1 ENGINE ICE DETECTION CONTROL, FUEL FIRE S/O VALVE, ENG 1, MAIN W/W AND CAC LIGHTS, FADEC GROUND PWR TEST ENG 1 CHAN B, TNK 1 TRANSFER PUMP AND APU SYS CONTROL IN CAC. AFT CARGO COMPT FAN INSPECTED WIRING AND FOUND WIRE G201-126-22C TO BE SERVICEABLE. PERFORMED SPLICE REPAIR OF WIRES G201-124-22A AND G201-125-22B JUST ABOVE FEED THRU P3-XVA IAW SWPM 20-10-01, AND PERFORMED CONTINUITY CENTER CARGO BAY JET PUMP SHUTOFF VALVE. PERFORMED SPLICE REPAIR OF WIRES G201-60-20 AFT CARGO PRESS REG VALVE PERFORMED SPLICE REPAIR OF WIRES G201-51-24, G201-52-24, G201-59-20 IAW SWPM 20-10-01. PERFORMED SPLICE REPAIR OF WIRES E111-78-16, E111-79-20, E111-82-16, E111-83-16, E111-84-20 AND RAN NEW WIRES THRU FEED THROUGH P3-XVA INTO LT MAIN WHEEL WELL AND SPLICED INTO CORRESPONDING LT OTBD AILERON DEFLECTION ACTUATOR PERFORMED SPLICE REPAIR OF WIRES E101-69-16RD, E101-69-16BL, E101-70-16RD, E101-70-16BL, AND ROUTED NEW WIRES TO LT WING DISCONNECT P1-818, IAW SWPM.
POST FLIGHT CHECK, FOUND L1 DOOR REMOTE PRESS INDICATOR WILL NOT ILLUMINATE. R & R BATTERIES AND OPS CHECKED OK. REF MM 25-61-04-4.
RT WING OTBD L/E REPAIRED IAW EA 1-5730-164851, 1-5730-164849, 1-5710-164853, 1-5710-164850, 1-5730-166316, 1-5730-164854.
ON TAKE OFF ROLL, AT APPROX 75 KTS, NR 1 THRUST REVERSER PRESSURE FAULT ILLUMINATED. REJECTED TAKE OFF. REPLACED PRESSURE REGULATING AND SHUTOFF VALVE IAW AMM 78-31-07-4-1.
PRESSURE FAULT. REMOVED REPLACED NR 1 THRUST REVERSER PRESSURE SWITCH PER AMM 78-31-08-2-1 OPS CHECKED NORMAL ACFT OK FOR SERVICE.
RTO DUE TO LEVEL 2 REVERSER FAILURE. FAULT WAS MOMENTARY AND DID NOT SPECIFY ENGINE. NO CURRENT OR LAST LEG FAULTS IN ECU 1A,B ECU 2A,B OR ECU 3A,B. OPERATED ALL REVERSERS IAW JRH 7-18, OPERATION AND INDICATIONS NORMAL. RAN ALL ENGINES IAW JRH CH6, BOOSTED ENGINES TO SAVE POWER LEVEL FOR ACFT LOCATION, NO FAULTS NOTED, ALL PARAMETERS AND INDICATIONS NORMAL.
LEFT WING INBD FLAP MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-00-01, REPAIR 1 FIG 201, REV 49. EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
RT WING ANTI-ICE TELESCOPIC DUCT CUTOUT AREA MISREPAIRED. CARRIED OUT REPAIR IAW EA 1-5740-160044. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
LT WING INBD FLAP, INBD SEGMENT UPPER SURFACE MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-00-01, REPAIR 2, FIG 201, REV 49. EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
MAIN DECK CARGO CENTER WING TANK UPPER SURFACES AT BS 1227, X= -68 TO X= -78 RT FOUND WITH SURFACE CORROSION. REPAIRED AS PER EA 1-5730-160042. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.
MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282HF IAW SNRM N00581. FOUND SEAT TRACK CORRODED ALONG FLANGE AREA BS 1683, X= -78. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1671 TO STA 1811 IAW SRM 53-00-52. FIG 201, REPAIR 1, REV 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FUSELAGE SKIN BS 295 MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-00-01, FIG 201. REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FRAME MISREPAIRED BS 535 LONGERON 24R. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FRAME MISREPAIRED BS 535. REPAIRED IAW SRM 53-20-07, FIG 201 REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FRAME MISREPAIRED BS 535. REPAIRED AS PER SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 49. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
MAIN DECK UPPER CARGO DOOR FORWARD HINGE SUPPORT 9TH LOBE HOLE FOUND EXCEED MAXIMUM PERMITTED LIMITS. REPAIR CARRIED OUT IAW EA 1-5230-159843. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 114.
ON REMOVAL OF FLOOR PANEL FOUND SEAT TRACK FLANGE WITH CORROSION AT RT BS 1781-1801, X= -77.25. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1671 TO 1811 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 755, X= 27.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 745 TO STA 765, X= 27.5 IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 49, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO COMPARTMENT CEILING AREA APPROX BS 715, X= 27.5. SEAT TRACK FOUND CRACKED. REPAIRED BY SECTONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 745, X= 27.5 IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REV 49. REFER TO SNRM N00523 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 715, X= 8.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 745 X= 8.5 IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 695, X= 27.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 745 X= 27.5 IAW SRM 53-00-52 FIG 201. REPAIR 1, REV 49. REFER TO SNRM N00523 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 635, X= 27.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 745, X= 27.5 IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 635, X= -27.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTONAL SEAT TRACK. REPLACEMENT FROM STA 585 TO STA 645, X= -27.5 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FORWARD CARGO BAY CEILING AREA APPROX BS 635, X= -8.5 FOUND SEAT TRACK CRACKED. REPAIRED BY SECTONAL SEAT TRACK. REPLACEMENT FROM BS 605 TO STA 645, X= -8.5 IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FUSELAGE SKIN MISREPAIRED. SKIN REPAIRED IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
LT WING T/E LOWER TEE FITTING FOUND CORRODED AT PANEL 641JB FORWARD CUT-OUT AREA. R & R IAW SRM 51-31-01 AND 51-33-01 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
NR 2 ENGINE AIR INTAKE INSIDE PANEL 363PL FOUND WIRE CUT-OUT INTERCOSTAL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02, FIG 201. REPAIR 2 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
TWO AREAS AROUND FASTENER HOLES HAS A CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA = 683.4 AND STA = 713.6. CARRIED OUT IAW EA 1-5710-159842. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
FUSELAGE SKIN FORWARD OF CARGO DOOR AFT FRAME DAMAGED, CARRIED OUT REPAIR IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 49.
DURING POST FLIGHT CHECK FOUND L-1 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE TEST LIGHT INOP. REPLACED BATTERIES, OPS CHECKS NORMAL IAW MM 25-61-06-5-0. FINAL CLOSED.
1R DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION SYS INOP. R & R LIGHT BULB ON RT PTT SWITCH IAW MM25-61-04-4. PERFORMED TEST IAW MM 25-61-04-5. TEST OK. MEL CLOSED. FINAL CLOSED.
DURING TRANSIT CHECK FOUND SLIDE PRESSURE PRESS-TO-TEST LIGHT INOP. RELEASED FOR SERVICE IAW MEL: 25-61-02. RELAMPED LT PRESSURE INDICATOR AND FUNCTION CHECKED PER MM 25-61-04-5-0. FOUND NORMAL. CLEARED DMI.
REJECTED TAKEOFF AT APPROX 120-130 KTS DUE TO COMPRESSOR STALL/ LOUD BANG. ENG 3 EXCEEDANCE REPORT, SHOWED PS3 OVER LIMIT. ALL OTHER PARAMETERS NORMAL, EGT NORMAL. STILL IN WORK. IAW AMM 72-00-05-6 FOR ENG NR 3 STALL INSP, FAN BLADE SHINGLING INSP CHECKED NORMAL, TAIL PIPE VISUAL CHECKED NORMAL, INLET AREA CHECKED NORMAL, EEC BITE TEST PASSED NO FAULT LOGGED. PERFORMED BORESCOPE INSP IAW MM 72-00-07, FOUND COMPRESSOR ROTOR BLADES STAGE 1 AND STAGE 12 OUT OF LIMITS. REMOVED POWERPLANT. INSTALLED NR 3 ENG IAW W/C 71T0903. RAN NR 3 ENG WITH POWER ASSURANCE TEST & ALL PARAMETERS CHECKED NORMAL IAW JRH.
AFTER TAKEOFF, GOT CAC DOOR LEVEL 1 ALERT. RETURNED AND LANDED WITHOUT INCIDENT. MX REPLACED CAC DOOR SWITCH IAW AMM 52-70-02.
AT FL340 "TANK 3 LOW" & "TANK TIP TRAPPED" NR 3. FUEL IN AUTO TRANSFERRED FROM TANK2 TO TANK3. TOTAL FUEL ONBOARD 18.0. ALERT TANK 2 LOW ILLUMINATED. "TANK 3 TIP TRAPPED ALERT" CAME ON A SECOND TIME AT FL280. DECLARED EMERGENCY AND LANDED MEM WITHOUT INCIDENT. WORK ACCOMPLISHED. OPENED PANEL 633AT IAW AMM 52-57-01 TO FOM. R & R NR3 6K FLOAT SWITCH IAW AMM 28-14-01. CLOSED PANEL IAW AMM 52-57-01. OPS & LEAK CHECK GOOD.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 281JF FOR SEAT TRACK ACCESS. FOUND SEAT TRACK STA 1741 X=75 OTBD FLANGE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1740-1 X= 75 O/B FLANGE REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1631 TO STA 1751 X= 75 IAW SRM 53-00-52, FIG 201. REPAIR REV 43. REFER TO SNRM N00894 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - FLOOR UNDERFLOOR SEAT TRACK INBD FLANGE STA 1199-1229 X=-8. FOUND MULTIPLE SURFACE CORROSION. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 43 THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 281GF FOR SEAT TRACK. REPAIR ACCESS FOUND SEAT TRACK STA 1581 X= 75 OTBD FLANGE WITH SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1581 X= 75 OTBD FLANGE REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1531 TO STA 1631 X= 75 IAW SRM 53-00-52, FIG 201. REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
01 EA FASTENER HOLE FOUND CRACK INDICATION DURING HFEC HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR CARRIED OUT AS PER EA 1-5710-140364. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 110.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 293EF FOR BLANKET REMOVAL. ACCESS FOUND FLOOR PANEL SUPPORT STA 1902-2007 X= 75 OTBD FLANGE WITH SURFACE CORROSION. MAIN DECK CARGO CORRODED FLOOR SUPPORT AT STA 1902 TO 2007 X= 75 R & R IAW SRM 51-31-014, REV 43. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551, REV G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 291FF FOR BLANKET REMOVAL, ACCESS FOUND SEAT TRACK STA 1853-1887 X= 75 OTBD FLANGE WITH SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1853 -1887 X= 75, OTBD FLANGE. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1751 TO STA 1887 X= 75 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - UNDERFLOOR SEAT TRACK INBD FLANGE STA 1481-1501 X= 107. FOUND MULTIPLE SURFACE CORROSION. CARRIED OUT REPAIR AS PER SRM 53-00-52 FIG 201 REPAIR 5, REV 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 281HF FOR SEAT TRACK REPAIR. ACCESS FOUND SEAT TRACK STA 1671 X= 75 OTBD FLANGE WITH SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1671 X=75 OTBD FLANGE REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1631 TO STA 1751 X=75 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAWGMM 6-2-100, REV 110.
MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 281GF FOR SEAT TRACK REPAIR. ACCESS FOUND SEAT TRACK STA 1601 X= 107 INBD FLANGE WITH SURFACE CORROSION. MAIN DECK CARGO STA 1601 X= 107 SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 43. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
LT WING - INBD LOWER SURFACE FOUND DENTS AT XIFH 146. LT WING INBD FLAP LOWER SKIN AND FILLER FABRICATED IAW SRM 57-50-01, FIG 201, REV 43. SKIN AND FILLER INSTALLED IAW SRM 51-35-01, REV 43. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - SUSPECT CRACK ON LONGERON SPLICE STA 5-113 TO 5-123 L-6. CRACKED LONGERON SPLICE REMOVED AT MAIN DECK CARGO LT STA 5-113 TO 5-123 L6 AREA IAW SRM 51-33-01, REV 43. NEW LONGERON SPLICE MACHINED IAW DWG A5A7112, REV D AND FPI CARRIED OUT IAW DPS 4-707, REV AW. NEW LONGERON SPLICE HOLES PICKED UP IAW SRM 51-21-01, REV 43 AND INSTALLED IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - SUSPECT CRACK FOUND ON LONGERON SPLICE STA 5-113 TO 5-123 L-7. CRACKED LONGERON SPLICE REMOVED AT MAIN DECK CARGO LT STA 5-113 TO 5-123 L7 AREA IAW SRM 51-33-01, REV 43. NEW LONGERON SPLICE MACHINED IAW DWG A5A7112 REV D AND FPI CARRIED OUT IAW D.P.S 4-707 REV. AW. NEW LONGERON SPLICE HOLES PICKED UP IAW SRM 51-31-01, REV 43. REPROTECTED NEW LONGERON SPLICE IAW SRM 51-21-01, REV 43 AND INSTALLED IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO - SUSPECT CRACK FOUND ON LONGERON SPLICE LT STA 5-113 TO 5-123, L-8. CRACKED LONGERON SPLICE REMOVED AT MAIN DECK CARGO LT STA 5-113 TO 5-123 L8 AREA IAW SRM 51-33-01, REV 43. NEW LONGERON SPLICE MACHINED IAW DWG ASA 7112, REV D AND FPI CARRIED OUT IAW DPS 4-707 REV AW. NEW LONGERON SPLICE HOLES PICKED UP IAW SRM 51-31-01 REV 43. PROTECTED NEW LONGERON SPLICE IAW SRM 51-21-01 REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
CRACK LINE-LT WING L/E ANTI ICE TELESCOPIC DUCT CUTOUT UPPER INBD CORNER EDGE. REPAIRED IAW SRM 57-40-01 REV 43, FIG 201. LT WING NR 3 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-5, REV 66. FOUND SATISFACTORY. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-10, REV 110.
SURFACE CORROSION - SEAT TRACK STA 1069 X=-8 IN MAIN DECK CARGO. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
NR 3 HYDRAULIC SYSTEM FAIL ALERT INFLIGHT. NR 3 SYSTEM LEAKED DOWN TO .1 GAL. AIRCRAFT LANDED MEM WITHOUT INCIDENT. LEAK COMING FROM NR 3 ENGINE PYLON FWD OUTBROAD SIDE OF LEADING EDGE SLAT PANEL. REMOVED AND REPLACED #3 ENG L/H AND R/H ENG HYD PUMPS DUE TO LOSS OF SYS 3 HYD IN FLIGHT. REF AMM 29-11-20-4. REMOVED AND REPLACED NR 3 ENG HYD FILTERS DUE TO LOSS OF NR 3 HYD SYS IN FLIGHT. REF AMM 29-12-41-2. DURING SERVICING AND LEAK CHK FOUND NR 3 PUMP SUCTION BLEED VALVE LINE CRACKED. REMOVED AND REPLACED LINE IAW MM REF 29-12-55-2. OPERATIONAL TEST, LEAK CHECK AND SERVICING ALL NORMAL. ITEM OK FOR SERVICE. ENGINE RAN PER JRH.
RIGHT WING INBOARD FLAP, FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM CENTER VANE TRACK TO OUTBOARD VANE TRACK AREA. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
UPON REMOVAL OF MAIN DECK FLOOR PANEL AT ZONE 230 FOUND SEAT TRACK CORROSION AT STATION 760 TO 765 X = -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE AT STATION 745 TO STATION 785, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CABIN, MAIN DECK SEAT TRACK BASE STATION 730 TO STATION 740, X = -8.5 FOUND CORROSION. CABIN, CORRODED SEAT TRACK AT STATION 730 TO STATION 740, X = -8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 605 TO STATION 745, X = -8.5 AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REFER TO SNRM NR N00637 FOR WORK DETAILS.
CABIN MAIN DECK SEAT TRACK AT STA 1210 X = 75.25 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO STATION 1269, X = 75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CABIN MAIN DECK SEAT TRACK AT STA 1531 TO STA 5-63 X = 75.25 FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-0 TO STATION 5-123, X = 75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
MAIN DECK UNDER FLOOR CENTER WING TANK TOP SURFACE, FOUND CORROSION AT STA 1230 X= -96. REPAIRED AS PER E.A. 1-5710-127427, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.
CABIN MAIN DECK STA 1970 TO STA 1980 X = 25, FOUND FLOOR SUPPORT WITH SURFACE CORROSION. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7087. HOLES PICKED UP AS PER SRM 51-31-01 VOLUME II. PROTECTED AS PER SRM 51-21-01 VOLUME II AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CABIN MAIN DECK SEAT TRACK AT STA 1480 TO STA 1500 X = 47.50 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1471 TO STATION 1531, X = 47.50 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
FORWARD CARGO COMPARTMENT AFT BULKHEAD STRUCTURE SUPPORT STANCHION CORRODED AT LBL 57 AFTER SIDEWALL PANEL REMOVED TO FACILITATE WIRING INSPECTION. FORWARD CARGO COMPARTMENT AFT BULKHEAD AT LBL 57 STRUCTURE SUPPORT STANCHION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
FORWARD CARGO COMPARTMENT AFT BULKHEAD STRUCTURE SUPPORT STANCHION CORRODED AT LBL 8 AFTER SIDEWALL PANEL REMOVED TO FACILITATE WIRING INSPECTION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. FABRICATED STANCHION AS PER DRAWING A6A7094. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.
FORWARD CARGO COMPARTMENT AFT BULKHEAD STRUCTURE SUPPORT STANCHION CORRODED AT LBL 29 AFTER SIDEWALL PANEL REMOVED TO FACILITATE WIRING INSPECTION. FORWARD CARGO COMPARTMENT AFT BULKHEAD STRUCTURE SUPPORT STANCHION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD, SPOT FACE INBOARD AND OUTBOARD SIDE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100
RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT INBOARD, SPOT FACE INBOARD AND OUTBOARD SIDE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLE NR B, AND NR C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE NR A. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CABIN, MAIN DECK SEAT TRACK BASE, STATION 615 TO STATION 625 X = -8.5 FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), UPPER ATTACHMENT OUTBOARD BORE FOUND CORROSION AT CHAMFER AREA. COMPLIED WITH E.A. 1-5750-127891, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), LOWER ATTACHMENT OUTBOARD BORE, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), LOWER ATTACHMENT INBOARD BORE, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT INBOARD, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100
SEAT TRACK BASE STATION 1114 TO STATION 1119 X = -8.5 FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CABIN, SEAT TRACK STATION 1089 X = 27.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
EMPENNAGE, AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 VERTICAL STIFFENER X = -11.18 UPPER AREA WAS FOUND CRACKED APPROXIMATELY 0.35 INCH. REPAIRED AS PER E.A. 1-5310-127892, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
A/P 1 KICKED OFF TWICE FL 360, GOT MOMENTARY FCC DATA FAULT ALERTS. A/P 2 OK, 5 MIN LATER GOT LVL 1 EMERG PWR ON ALERT, RECYCLED EMER PWR SW, ALERT RETURNED. DEPLOYED ADG, SELECTED ELEC MODE. DIVERT TO DEN. ON FINAL SLOWING THROUGH 170 KIAS A/P AND ATT FAILED LOST LEFT EMERGENCY BUS. INTEROGATED CFDS, EPCU FAULTED EMERG POWER RELAY INTERFACE. T/S PER MD11 FIM . FOUND RCCB FOR LT DC EMERG BUS B1-1754 OPEN AND SIGNS OF OVERHEATING AT TERMINAL A1. REMOVED AND REPLACED C/B B1-1754 (LEFT EMERG DC FEED C/B). OPS CHECK NORMAL FOR LT EMERG BUSS AND EMER PWR TEST. FCC 1 RTS IS NORMAL. RETURNED A/C TO SERVICE.
DURING INSPECTION ON TRIMMED AREA ON NOSE LANDING GEAR RIGHT SIDE TRUNNION FITTING, 03 EACH CRACKS FOUND ON LONGERON FROM LOWER FASTENER HOLE COMMON TO THE REPAIR AREA. [08-17-07] REPAIRED AS PER FEDEX EA 1-5310-112374, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LT WING, LEADING EDGE EXTERIOR SKIN BETWEEN SLAT TRACK NR 10 AND NR 11 FOUND CHIPPED. [08-17-07] CHIPPED AREA SMOOTHENED OFF AS PER SRM 51-21-01 VOLUME II. EXCEEDED LIMIT AS PER SRM 57-00-01 FIGURE 2 VOLUME I. REWORKED AREA REPAIRED AS PER SRM 57-10-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK INDICATIONS REVEALED IN 09 EA FASTENER HOLES TOWARDS EDGE OF ACCESS. C/OUT IN RT WING LWR SKIN ACCESS DOOR C/OUT (BETWEEN STA XORS= 683.400 TO XORS= 713.600). [08-17-07] REPAIRED AS PER FEDEX EA 1-5710-112376, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK INDICATIONS REVEALED IN 06 EA FASTENER HOLES TOWARDS EDGE OF ACCESS C/OUT IN LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS= 683.400 TO XORS= 713.600. REPAIRED AS PER FEDEX EA 1-5710-112375, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
ENG NR 3: AFTER ENGINE REMOVAL FOUND PYLON FWD MOUNT LT MOUNT LT AFT BORE HOLE, SUSPECT PITTING CORROSION. [08-20-07] REPAIR CARRIED OUT AT ENG NR 3 PYLON FWD MOUNT LH AFT BORE HOLE AS PER FEDEX EA 1-5410-112377, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730-114786, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
NOSE LANDING GEAR RT TRUNNION FITTING CRACKED. [08-20-07] REPAIRED AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS AS REQUIRED IN SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFTER CENTER CARGO CEILING PANEL REMOVED, FOUND MAIN DECK CARGO SEAT TRACK AT STA 1815, X = -27.5 CORRODED. [08-15-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFTER CEILING PANEL REMOVED, FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1756, X = -8.5 CORRODED. [08-15-07] REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730-114787, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LT WING, I/B FLAP LOWER SKIN (I/B HALF) FOUND WITH NUMEROUS DENTS. [08-15-07] REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
NOSE LANDING GEAR LT TRUNNION FITTING FOUND CRACKED. [08-20-07] REPAIRED AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS REQUIRED IN SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FORWARD CABIN , FOUND CARGO SEAT TRACK AT STA 500 RBL 62" WORN.
AFT CARGO COMPARTMENT, RT TUNNEL AREA LONGERON 38R SPLICE BETWEEN STA 1853 TO STA 1871 FOUND CRACKED. [08-15-07] REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RT WING LEADING EDGE CAVITY STRINGER AT XOS 789 FOUND CRACKED. [08-17-07] REPAIRED AS PER FEDEX E.A. 1-5710-112372, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
HYD 3 FAIL, QTY .1 LOWERED GEAR VIA ALTERNATE EXTENSION FOUND LEAK IN CENTER GEAR AT HYD LINE ADJACENT TO RMPS. REPAIRED CRACK AT FERREL WITH RYNGLOK PER MM 20-10-01-2. SERVICED NR 3 HYD RESERVOIR TO FULL AND LEAK CHKS OK PER SMP. NEED ALTERNATE RELEASE CONTROL LEVER NOSE/MAIN GEAR STOWED. RESET ALTERNATE GEAR EXTENSION LEVER PER REF TO MD-11 WORK CARD 32T3601 REVISION NR 0001, 11-FEB-2004. SYSTEM OKAY FOR SERVICE AT THIS TIME.
RT WING I/B FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING INBOARD FLAP VANE LOWER SURFACE REPAIRED AS PER FEDEX EA NR1-5750-94612, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT INBOARD FLAP VANE SKIN DELAM REPAIR. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 1470, X=8.5 RT) FOUND EDGE CORRODED. MAIN DECK CARGO SEAT TRACK REPAIR CARRIED OUT FROM STA 1410 TO STA 5- 0 RT X=8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 5/0, X=75.25 RT) FOUND EDGE CORRODED. MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 1390 TO STA 5/0 RT X=75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 939, X=47.5 LT) FOUND EDGE GOUGED. MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 890 - STA 950 LT X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 939, LH X=27.5) FOUND EDGE GOUGED. MAIN DECK CARGO SEAT TRACK (STA 939, LH X=27.5) EDGE GOUGED MARK REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.050", MATERIAL REMAINING =0.030" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 910 TO STA 970 LH X=27.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 1521, X=47.5 RT) FOUND EDGE GOUGED. MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 1421 TO STA 5-0 RT X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO CENTER WING TANK UPPER PANEL (STA 1230, FROM X=75.25 LT TO X=107.25 RT) FOUND TOP SKIN HI-LOCK SURROUNDING CORRODED. REPAIR CARRIED OUT IAW FEDEX EA 1-5710-95796, WINGS CENTER WING TANK UPPER SKIN PANEL CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 1341, X=8.5 RT) FOUND CORRODED. MAIN DECK SEAT TRACK REPAIRED FROM STA 1229 TO STA 1370 RT X=8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 900, RH X=47.5) FOUND EDGE GOUGED. MAIN DECK CARGO SEAT TRACK (STA 900, RH X=47.5) EDGE GOUGED MARK REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.040", MATERIAL REMAINING =0.040" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 890 TO STA 929 RH X=47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK (STA 899-910, LH X=47.5) FOUND EDGE GOUGED. MAIN DECK CARGO SEAT TRACK (STA 899-910, LH X=47.5) EDGE GOUGED MARK REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.050", MATERIAL REMAINING =0.030" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 890-950, LH X=47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 755-765, LH X=47.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 755-765, LT X=47.5 EDGE GOUGE MARK REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.050", MATERIAL REMAINING =0.030" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. SEAT TRACK FROM STA 725 TO STA 765 LT X=47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1321 TO 1381, LT X=8.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1321 TO 1381, LT X=8.5 CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS=0.080" MATERIAL REMOVED=0.035", REMAINING THICKNESS=0.045" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1401-1501, LT X=8.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1401-1501, LT X=8.5 NUT CLIP MOUNTING HOLE SURROUNDING CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.100", MATERIAL REMOVED =0.060", MATERIAL REMAINING =0.040" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1390 TO STA 5-0 LT X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1581, LH X=8.5 FOUND CORRODED. SNRM N00959: MAIN DECK CARGO SEAT TRACK AT STA 1581-1600, LH X=8.5 EDGE CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.040", MATERIAL REMAINING =0.040" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1531 TO STA 1633 LH X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1230, RH X=8.5 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.030", THICKNESS REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1129 TO STA 1370 RH X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1, VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 5/34, RH X=8.5 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.100", MATERIAL REMOVED =0.050", MATERIAL REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I SEAT TRACK FROM STA 5-0 TO STA 1531 RH X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1435, RT X=47.5 FOUND EDGE GOUGED. GOUGED REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.050", MATERIAL REMAINING =0.030" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1421 TO STA 5-0 RT X=47.5 CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1301-1341, RT X=75.25 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1301-1341, RT X=75.25 NUT CLIP MOUNTING HOLE SURROUNDING CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL THICKNESS =0.040", MATERIAL REMAINING =0.040" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1265 TO STA 1390 RH X=75.25 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1481-5/0, RT=75.25 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1481-5/0, RT=75.25 NUT CLIP MOUNTING HOLE SURROUNDING CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.030", MATERIAL REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1390 TO STA 5/0 RT X=75.25 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 5/11-5/53, LH X=8.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 5/11-5/53, LT X=8.5 CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.035", THICKNESS REMAINING =0.045" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 5-0 TO STA 1531 LT X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1401-1481, LH X=75.25 FOUND CORRODED. MAIN DECK CARGO LT X=75.25 FROM STA 1390 TO STA 5-0 SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II MATERIAL REMOVED =0.050", ORIGINAL THICKNESS = 0.100", MATERIAL REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1240, LH X=8.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1240, LT X=8.5 CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS=0.080" MATERIAL REMOVED=0.030", REMAINING THICKNESS=0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1410-1481, RH X=8.5 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK AT STA 1410-1481, RH X=8.5 NUT CLIP MOUNTING HOLE SURROUNDING CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.030", MATERIAL REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 1410 TO 5-0 RH X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STA 1059, RIGHT X =8.5 FOUND CORRODED. FOUND MAIN DECK CARGO SEAT TRACK AT STA 1059, RIGHT X =8.5 SURFACE CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL EDGE REMOVED = 0.006" FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
RIGHT HAND WING O/B FLAP I/B AFT HINGE BRACKET FWD ATTACHMENT O/B AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-95793.
MAIN DECK CARGO SEAT TRACK (RT X=75.25 STA 5/53) FOUND EDGE UNDER FLOOR CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED =0.030", MATERIAL REMAINING =0.050" AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. SEAT TRACK FROM STA 5-0 TO STA 1531 RH X=75.25 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME II. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING O/B FLAP I/B AFT HINGE BRACKET FWD ATTACHMENT I/B CENTER HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-95793.
RT WING OB FLAP IB AFT HINGE BRACKET FWD ATTACHMENT OB CENTER HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-95793. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
RT EXTERIOR STRINGER (LONGERON 28) UNDER R3 DOOR SCUFF PLATE FOUND CORRODED. REPAIR CARRIED OUT AT FUSELAGE RT EXTERIOR STRINGER (LONGERON 28) UNDER R3 DOOR SCUFF PLATE CORRODED AREA AS PER FEDEX EA NR 1-5310-95798, TITLE: "FUSELAGE MAIN FRAME LONGERON S28 (RIGHT) AT STATION Y=1259 THROUGH Y=1265, CORROSION BLEND OUT". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LT EXTERIOR STRINGER (LONGERON 28) UNDER L3 DOOR SCUFF PLATE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-95797, FUSELAGE MAIN FRAME, LONGERON 28-L AT STATION Y=1293 THROUGH Y=1315, CORROSION BLEND OUT AND CRACK REPAIR. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
LT WING REAR SPAR CAP UPPER SURFACE FOUND WITH CORROSION AT XORS 1042. LT WING REAR SPAR CAP UPPER SURFACE AT XORS 1042 CORROSION REMOVED AND FOUND BEYOND ALLOWABLE LIMITS AS PER SRM 57-20-00 FIGURE 6 VOLUME I. ORIGINAL THICKNESS =0.137", MATERIAL REMOVED =0.035", REMAINING THICKNESS =0.102". REWORK AREA REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5710-95792, TITLE: WINGS, LEFT REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1042 ROUGH XORS = 1051 REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RT WING REAR SPAR CAP UPPER SURFACE FOUND WITH CORROSION AT XORS 1040. RT WING REAR SPAR CAP UPPER SURFACE XORS 1040 CORROSION AREA REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5710-95791, TITLE: WINGS, RIGHT REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1040 THROUGH = 1051 REPAIR. ORIGINAL THICKNESS =0.126", MATERIAL REMOVED =0.054", REMAINING THICKNESS =0.072". THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
CARGO SEAT TRACK (STA 1581, RH X=8.5) FOUND CORRODED. MAIN DECK CARGO SEAT TRACK (STA 1581, RH X=8.5) SURFACE CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. ORIGINAL THICKNESS =0.080", MATERIAL REMOVED = 0.050", MATERIAL REMAINING = 0.030". SEAT TRACK FROM STA 1531 TO STA 1590 RT X=8.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING TANK STRINGER 14 FOUND CRACK DURING HFEC INSPECTION. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING TANK STRINGER 43 FOUND CRACK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING TANK STRINGER 42 FOUND CRACK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LEFT WING TANK STRINGER 14 FOUND CRACK DURING HFEC INSPECTION. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING TANK STRINGER 44 FOUND CRACK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING TANK STRINGER 42 FOUND CRACK DURING HFEC INSPECTION. CRACK REPAIRED AS SRM 57-20-00 FIGURE 10 VOLUMEI. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING TANK STRINGER 10 FOUND CRACK DURING HFEC INSPECTION. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING TANK STRINGER 12 FOUND CRACK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING TANK STRINGER 13 FOUND CRACK DURING HFEC INSPECTION. CRACK REPAIRED AS SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING TANK STRINGER 11 FOUND CRACK DURING HFEC INSPECTION. CRACK REPAIRED AS SRM 57-20-00 FIGURE 10 VOLUMEI. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT HAND FIXED L/E RIG ANGLE FOUND CRACKED AT XORS 475. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. ANGLE FABRICATED AS PER DWG ARB2931.
LEFT WING LEADING EDGE BEADED DOUBLER AT XOS 707 FOUND CRACKED. CARRIED OUT AS PER FEDEX EA 1-5730-98787.
LEFT WING LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED AROUND FASTENERS. REPAIR CARRIED OUT IAW FEDEX EA 1-5730-98788.
RIGHT HAND WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XORS 542. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-95786.
RIGHT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA #1-5740-94613, TITLE: WINGS. LEADING EDGE AND LEADING EDGE DEVICES, RIGHT FIX LEADING EDGE SKIN REPAIR XORS = 464.000 THROUGH XORS = 475.000. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT HAND WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XORS 522. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-95786 PT1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK.
LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK.
LEFT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK.
RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE:WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK..
LEFT HAND WING UPPER STRINGER (S13) END FOUND CRACKED AT INSIDE ACCESS PANEL 535BT. LEFT HAND WING UPPER STRINGER (S13) SLOT OUT CRACKED AREA AT STRINGER END AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I.
SNRM N0896: LT WING UPPER STRINGER (S12) END FOUND CRACKED AT INSIDE ACCESS PANEL 536AB. REPAIR CARRIED OUT AT LEFT HAND WING UPPER STRINGER 12 END AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I.
CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER SUSPECT CRACKED. CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. LEFT HAND SPOILER CONTROL PUSHROD "DU" AND "MO" ADJUSTED AS PER AMM 27-61-00-830-006 AND AMM 27-61-00-830-017. OPERATION CHECK CARRIED OUT FOUND 'SATIS' AS PER AMM 27-61-00-730-801.
LEFT HAND WING UPPER STRINGER (S11) END FOUND CRACKED AT INSIDE ACCESS PANEL 536CB. REPAIR CARRIED OUT AT LT WING STRINGER 11 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I.
SNRM N0631: MAIN DECK, SEAT TRACK RBL 47.5 CRACKED AT STA 5-53. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 SHT 1 VOL I.
MAIN DECK, HAT SECTION CORRODED AT STA 1887 RBL 17 AFTER FLOOR PANEL 293BF REMOVED FOR FABRICATION. MAIN DECK, CORRODED HAT SECTION AT STA 1887 RBL 17 REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED AND REWORKED AS PER DWG AGA7087 PAINT TOUCHED UP AND PART MARKED AS PER SRM 51-21-01 VOL II GMM 7-0-1001. NEW HAT INSTALLED AS PER SRM 51-31-01 VOL II.
NR 26 RIGHT HAND BARREL NUT BORE FOUND CRACKED AT BOTTOM INBOARD SIDE AREA. NR 26 RIGHT HAND BARREL NUT BORE SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.
RIGHT HAND WING UPPER STRINGER END (S10) FOUND CRACK INSIDE FUEL TANK ACCESS PANEL 638AB. RIGHT HAND WING UPPER STRINGER END (S10) TRIMMED OUT CRACKED AREA AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 AND SRM 57-20-00 FIG 10 VOL I.
LEFT HAND WING (S10) STRINGER END FOUND CRACK INSIDE FUEL TANK PANEL 538AB. STRINGER NR 10 CRACK REMOVED AS PER SRM 57-20-00 FIG 10 VOL I & INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II & SRM 57-20-00 FIG 10 VOL I.
RT WING OUTBOARD FLAP INBOARD HINGE (AIRCRAFT SIDE) ACTUATOR INBOARD AND OUTBOARD LUG HOLES CORRODED AREA REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69233 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.
LT WING, O/B FLAP O/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT, AFT BOLT HOLE CORRODED. O/B FLAP O/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT AFT BOLT HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68412 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT COOROSION.
LT WING- L/E XORS 805, CRACK FOUND APPROX 12 INCHES FROM TOP TO LOWER SURFACE. REPAIR CARRIED OUT AT LT WING L/E XORS 805 TOP TO LOWER SURFACED AREA AS PER SRM 57-10-00 FIG.7 VOL.I.
RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE), FWD ATTACHING POINT, I/B FWD BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP O/B HINGE (FLAP SIDE) AFT ATTACHING POINT, AFT BOLT HOLE CORRODED. ** S/D ** COMING
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHMENT POINT AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LEFT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT, O/B CTR BOLT, HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B CTR BOLT HOLE FOUND CORRODED. ** S/D ** COMING
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR
LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT, O/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR
LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT, I/B FWD BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B CTR BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT I/B CTR BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR .
RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHMENT POINT FWD BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP O/B HINGE (FLAP SIDE), FWD ATTACHING POINT, I/B AFT BOLT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT O/B AFT BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED. R/R PER EA 1-5750-69247.
LT WING O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE CORRODED.
LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE) FWD ATTACHING POINT, O/B AFT BOLT HOLE CORRODED. SNRM N1126 - LT WING- O/B FLAP I/B HINGE (FLAP HINGE SIDE) FWD ATTACHING POINT O/B AFT BOLT HOLE REPAIR CARRIED OUT IAW E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE), AFT ATTACHING POINT, BOTH FWD AND AFT BOLT HOLE CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP HINGE SIDE) AFT ATTACHING POINT, BOTH FWD AND AFT BOLT HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413, WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT COOROSION.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE) AFT ATTACHING POINT BOTH FWD AND AFT BOLT HOLES CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
RT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.
LT WING- O/B FLAP I/B HINGE (AIRCRAFT SIDE), ACTUATOR I/B AND O/B LUG HOLES CORRODED. TRAILING EDGE & TRAILING EDGE DEVICES- LH OUTBD FLAP INBD HINGE BRACKET REPAIR.
LT WING- O/B FLAP L/E STOP BOLT SUPPORT ISLAND FOUND CRACKED.
RT WING- O/B FLAP L/E STOP BOLT SUPPORT ISLAND FOUND CRACKED.
LT WING- O/B FLAP O/B HINGE (AIRCRAFT SIDE), ACTUATOR I/B AND O/B LUG HOLES CORRODED. AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-69234 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES- LH OUTBD FLAP OUTBD HINGE BRACKET REPAIR.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
RT WING- I/B FLAP O/B HINGE (FLAP SIDE), LWR PIVOT I/B LUG HOLE CORRODED. SNRM N1013 - RH WING- I/B FLAP O/B HINGE (FLAP SIDE) LWR PIVOT I/B LUG HOLE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-68411, WING- RIGHT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED.
LT WING- IB FLAP OB HINGE (FLAP SIDE) LWR ATTACHING PIVOT OB LUG HOLE FOUND CORRODED. LT WING- I/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE. REPAIR CARRIED OUT IAW EA 1-5750-68410 WINGS-LEFT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED.
RT WING - O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT, I/B LUG I/B FACE FOUND CORRODED. RT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG I/B FACE CORROSION AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68414 WINGS- RIGHT O/B FLAP- O/B HINGE AFT SUPPORT CORROSION.
RT WING - O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG I/B FACE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG I/B FACE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
RT WING - O/B FLAP I/B HINGE (FLAP SIDE), LWR PIVOT, I/B LUG HOLE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT, I/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
RT WING - O/B FLAP I/B HINGE (FLAP SIDE), LWR PIVOT O/B LUG HOLE CORRODED. RT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68415 WINGS- RIGHT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
RT WING - O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE FOUND CORRODED. RT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-69232 WINGS- TRAILING EDGE & TRAILING EDGE DEVICES- RH OUTBD FLAP OUTBD HINGE BRACKET REPAIR.
LT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE FOUND CORRODED. LOWER ATTACHING PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68412 WINGS- LT O/B FLAP- O/B HINGE AFT SUPPORT CORROSION.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LEFT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LT O/B FLAP- I/B HINGE AFT SUPPORT CORROSION.
DURING REMOVAL OF CARGO HANDLING TRAY CORROSION OBSERVED ON FLOOR STRUCTURE AT STA 1961 LBL 58 IN CABIN.
CABIN- EXFOLIATION CORROSION OBSERVED ON SEAT TRACK UPPER LEG AT STA 1383 RBL 9.
LT WING- NR 16 L/E SLAT TRACK I/B SUPPORT RIB FOUND CRACKED.
RT WING- NR 16 L/E SLAT TRACK I/B SUPPORT RIB FOUND CRACKED.
UPON GEAR RETRACTION, RIGHT MLG LIGHT STAY ILLUM ON BOTH PRIMARY AND SECONDARY GEAR DISPLAYS.
CENTER GEAR AIRFRAME SIDE LT PILLOW BLOCK FITTING HAS CORROSION PITTING AT MATING SURFACE AND GUIDE PIN HOLE. REMOVED AND REPLACED PER SRM 53-40-00.
FUSELAGE EXT SKIN DENTS BETWEEN Y STA 275-313, X LONGERON 23-24 LT. TRIMMED OFF AND FAB REPAIR DOUBLER AND INNER FINGER DOUBLER, INSTALLED PER SRM 53-20-00 FIG 2 VOL 1.
MAIN DECK, SEAT TRACK FOUND CRACK AT BS 755 X=8.5 RT. *S/D* REPAIRED, FABBED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL 1.
MAIN DECK, SEAT TRACK FOUND CRACK AT BS 755 X=27.5 RT LENGTH 3 IN. *S/D* REPAIRED PER SRM 53-70-00 FIG 1 VOL 1. REPAIRED SPLICE AND TRACK AS PER SRM 53-70-00. REPAIR PARTS INSTALLED.
HNL - FLIGHT CREW HEARD LOUD BANG ON GEAR RETRACTION AFTER TAKEOFF. ON ARRIVAL NAN, RT NOSE WHEEL TREAD WAS FOUND SEPARATED AND CAUSED DAMAGE TO RT GLIDE PATH ANTENNA, ILS REFLECTOR AND NOSE WHEELWELL CEILING INSULATION BLANKET. RIGHT NOSE WHEEL REPLACED, PORTION OF BLANKET REMOVED AND NR 2 ILS SYSTEM ON MEL. AIRCRAFT RETURNED TO SERVICE.
EXCESSIVE FREE PLAY IN HORIZ STAB RT JACK SCREW NUT. CHANGE RT HORIZ STAB JACK SCREW REF M/M 27-44-04-4 PERFORM ADJUST AND TEST PER MM 27-40-00-5. ALL BEAR AND BUSH CK WITHIN LIMIT PER DAC DRAWINGS ALC 8050 AND AJH 7135.
ON T/O AT FLAPS UP TRIM JAM AT 7.2 DEG NOSE UP. BOTH PICKLE SWITCH AND MANUAL TRIM SUITE CASE HANDLES, BUT NO MOVEMENT. CKD CIRCUIT BREAK AND RAN STAB INOP (2.5-12) NO HELP. TRIED BOTH AUTOPILOT, NO HELP. DUMP 110,000 LBS OF FUEL AND RETURN TO KANSAI. ON FINAL TRIED ELEV FEEL SWITCH BUT DIDN'T HELP LAND WITH 28 DEG FLAPS MED BRAKE LAND WAS NORMAL (458,000 LBS). ON BLOCK IN POST FLT CREW COULD SEE NOTHING VISUALLY WRONG WITH STAB FND LT HORIZ STAB ACTUATOR ASSY AS FAULTY AND FUSE PIN WAS SHEARED ON STAB CHAIN DRIVE ASSY. REMOVED AND REPLACED LEFT HAND ACTUATOR ASSY PER EA 1-2740-29542 AND REMOVED AND REPLACED DRIVE UNIT PER M/M 27-44-06-4. HORIZ STAB OPS NORM PER M/M 27-340-00-5. FCC 1 AND 2 AFS STAB R-
GEN 3 OFF LIGHT ON CLIMBOUT VOLTS O/FREQ 400,1 RESET ATTEMPTED. SEE PREVIOUS. PERFORMED T/SHOOTING PE. 3-13 WAS OPEN. REMOVED AND REPLACED NR 3 IDG PER MM 24-21-02. RUN ENGINE CHECKED OPERATION OF NR 3 IDG, FOUND NORMAL PER JRH MD-11.
ENGINE FAILED INSP PER EA 1-7220-31514, INSP OF FIRST STAGE BOOSTER VANES. FOUND NUMEROUS LOOSE AND MISSING FASTENERS BOOSTER CASE CRACKED IN SEVERAL PLACES. REMOVED AND REPLACED NR 2 ENGINE. RII COMPLETED, ENG RUN, LEAK AND OPS CHECK GOOD.
INSP OF THE FIRST STAGE BOOSTER VANES, EA 1-7220-31513, EA COMPLETED ON NR 1 ENG, FOUND 22 MISSING FASTENERS AND SEVERAL CRACKS IN STATOR CASE. REMOVED AND REPLACED NR 1 ENG PER WORK CARD 29T0301, 54T0201, 71T0101, 71T0701 AND FEC -M-3238, OPS CK AND LEAK CK GOOD.
THIS A/C HAD THE NR 2 IDG DEFERRED. IN FLIGHT THE NR 3 IDG WENT INOP, THE CREW DID AN AIR TURNBACK INTO NADI. PER THE MEL YOU CANNOT DEFER TWO IDG AT THE SAME TIME. REMOVED AND REPLACED THE NR 3 IDG.
DURING OPS CK OF NOSE WHEEL STEERING, THE RT STEERING CYLINDER BLEW APART (LITERALLY). ** (S/D) ** REMOVED AND REPLACED RT NOSE WHEEL STEERING CYLINDER PER MM 32-52-30. S/N OFF AP214, S/N ON FEC101.