N583FE
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 CORPORATION (FDEA) | Operator | on 2020-06-03 | Operator named in NTSB report |
Accident & incident history
Operated by Federal Express (per NTSB report)
Operated by FEDERAL EXPRESS CORP (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
460 reports on file, 1997-12-12 – 2026-07-29.
Part: HYDRAULIC SYSTEM — FAILED (ZONE 100) · airframe 100,248 hrs · 23,835 cycles
FLIGHT STARTED WITH MEL 29-08-01-01 OPERATING WITH HYD MANUAL. PASSING THROUGH APPROXIMATELY 5000 FT, HYD 2L OFF ALERT CAME ON. SYS WENT TO 2R AND WITHIN 10 SECS IT FAILED ALSO. BOTH RMPS WERE ON FROM T/O. DECLARED AN EMERGENCY & RETURNED TO MEMPHIS. PERFORMED HSC RTS LIKE PREVIOUS WRI 29-11/7046, RAN THROUGH ALL OPS OF PUMPS/LRUS CONTROLLED BY THE HSC, NO FAULTS. FOLLOWED FIM TASK 29-10-06, RAN NR 2 ENGINE 30 MINS WITH NO FAULTS, HYD TEMPS STARTED AT 46*C AT BEGINNING OF RUN & CLIMBED TO A MAXIUM OF 67*C DURING 30 MIN ENG RUN, FIM TASK TEMP THRESHOLD IS 100*C BEFORE COMPONENTS OR OTHER REQUIRMENTS NEEDED TO BE MET. ALL TESTS PASSED IAW FIM. PERFORMED OPS CHECKS IAW 29-12-00, NO FAULTS FOUND.
Earlier reports · 1997–2025 · 459 reports
2025
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 100,071 hrs · 23,777 cycles
UPON EVALUATION FOUND EXISTING DOUBLER REPAIR ON FUSELAGE SKIN STATION 999 TO 1009 BETWEEN RIGHT HAND LONGERON 31 TO LONGERON 33 DOES NOT COMPLY TO CURRENT SRM 53-00-15-2R REPAIR 8 FIGURE 202. FUSELAGE SKIN AT STATION 999 TO STATION 1009 BETWEEN RIGHT HAND LONGERON 31 TO LONGERON 33 EXISTING REPAIR DOUBLER REMOVED AS PER MD-11 SRM 51-33-01-0G. REPAIR CARRIED OUT AS PER MD-11 SRM 53-00-15-2R REPAIR 8 FIGURE 202. REPETITIVE INSPECTION REQUIRED- INITIAL INSPECTION AT 4000 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 4000 FLIGHT CYCLES BY EXTERNAL VISUAL METHOD AS PER MD-11 SRM 53-00-15--2R FIGURE 202 TABLE 201 REPAIR 8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
RIGHT FLOOR PANEL 272GF AT STATION 1437, X= -47.5 TO X= -75.25 MAIN LANDING GEAR VIEW WINDOW ACCESS CUT OUT FOUND DELAMINATED. CABIN-RIGHT HAND DELAMINATED FLOOR PANEL NUMBER 272GF AT STATION 1437, X=-47.5 TO X= -75.25 MAIN LANDING GEAR VIEW WINDOW ACCESS CUTOUT, REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
LEFT FLOOR PANEL 271GF AT BS 1437, X=47.5 TO X=75.25 MAIN LANDING GEAR VIEW WINDOW ACCESS CUT OUT FOUND DELAMINATED. CABIN-LEFT HAND DELAMINATED FLOOR PANEL 271GF AT STATION 1437, X=47.5 TO X=75.25 MAIN LANDING GEAR VIEW WINDOW ACCESS CUTOUT, REMOVED AND REPLACED IAW AMM 53-21-04-4. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005, REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FRAME SPLICE — CRACKED (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN-INTERIOR FUSELAGE FRAME AT LEFT HAND STATION 1761 LONGERON 14 FOUND SPLICE ANGLE CRACKED APPROXIMATELY 0.4". FUSELAGE FRAME AT LEFT HAND STATION 1761 LONGERON 14 CRACKED SPLICE ANGLE REMOVED AND REPLACED AS PER MD -11 SRM 51-31-01-OG. SPLICE ANGLE FABRICATED AS PER DOUGLAS DRAWING AFA0029 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1239 X=27.5 FOUND CROWN WORN. SEAT TRACK STATION 1239, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 1209 TO EXISTING SPLICE STATION 1249, X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1501, X=8.5 FOUND CROWN WORN. SEAT TRACK STATION 1501, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1471 TO STATION 1531/5-0, X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1156, X=47.5 FOUND CROWN WORN. SEAT TRACK STATION 1156, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION EXISTING SPLICES STATION 6-100/1129 TO STATION 1189, X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1541, X=-47.5 FOUND CROWN WORN. SEAT TRACK STATION 1541, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 1571 TO EXISTING SPLICE STATION 5-123/1531, X= -47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1501, X=-8.5 FOUND CROWN WORN. SEAT TRACK STATION 1501, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1451 TO STATION 1531/5-0, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1234, X=-8.5 FOUND CROWN WORN. SEAT TRACK STATION 1234, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXIISTING SPLICES STATION 1209 TO STATION 1269, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1357, X=-8.5 FOUND CROWN WORN. SEAT TRACK STATION 1357, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXIISTING SPLICES STATION 1351 TO STATION 1391, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 5-4, X=27.5 FOUND CROWN WORN. SEAT TRACK STATION 5-4, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1531/5-0 TO STATION 5-43, X= 27.5.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1357, X=47.5 FOUND CROWN WORN. SEAT TRACK STATION 1357, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 1371 TO EXISTING SPLICE STATION 1311, X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 6-5, X=-27.5 FOUND CROWN WORN. SEAT TRACK STATION 6-5, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 6-60 TO EXISTING SPLICE STATION 6-0/1129, X= -27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1234, X=8.5 FOUND CROWN WORN. SEAT TRACK STATION 1234, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES BS 1249 TO 6-100/1129, X= 8.5 IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT BELT — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1150, X=-47.5 FOUND CROWN WORN. SEAT TRACK STATION 1150, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXIISTING SPLICES STATION 6-100/1129 TO STATION 1169, X= -47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 5-43, X=-8.5 FOUND CROWN WORN. SEAT TRACK STATION 5-43, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXIISTING SPLICES STATION 1531/5-0 TO STATION 5-63, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 5-4, X=47.5 FOUND CROWN WORN. AT SEAT TRACK STATION 5-4, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 5-63 TO EXISTING SPLICE STATION 1531/5-0, X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1154, X=8.5 FOUND CROWN WORN. SEAT TRACK STATION 1154, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXIISTING SPLICES STATION 1249 TO STATION 6-100/1129, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN-SEAT TRACK AT STATION 5-4, X=8.5 FOUND CROWN WORN AS MARKED. CABIN-AT SEAT TRACK STATION 5-4, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 5-43 TO STATION 5-0/1531, X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 6-5, X=27.5 FOUND CROWN WORN. SEAT TRACK STATION 6-5, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 6-60 TO EXISTING SPLICE STATION 6-0/1129, X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1357, X=27.5 FOUND CROWN WORN. SEAT TRACK STATION 1357, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1371 TO STATION 1311, X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1541, X=-27.5 FOUND CROWN WORN. SEAT TRACK STATION 1541, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 1571 TO EXISTING SPLICE STATION 5-123/1531, X= -27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 6-5, X= -8.5 FOUND CROWN WORN AS MARKED. CABIN-AT SEAT TRACK STATION 6-5, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1129/6-0 TO STATION 6-60, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 1150, X=27.5 FOUND CROWN WORN. SEAT TRACK STATION 1150, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 6-100/1129 TO STATION 1169, X= 27.5.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1154, X=-27.5 FOUND CROWN WORN. SEAT TRACK STATION 1154, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 6-100/1129 TO STATION 1209, X= -27.5.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT BS 1357, X=8.5, FOUND CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN BS 1391 TO EXISTING SPLICE BS 1351, X= 8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN SEAT TRACK AT STATION 6-5, X=47.5 FOUND CROWN WORN. SEAT TRACK STATION 6-5, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 6-60 TO EXISTING SPLICE STATION 6-0/1129, X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
CABIN-SEAT TRACK AT STATION 6-5, X=8.5 FOUND CROWN WORN AS MARKED. CABIN-AT SEAT TRACK STATION 6-5, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 6-60 TO EXISTING SPLICE STATION 1129/6-0, X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1234, X= -27.5 FOUND CROWN WORN. SEAT TRACK STATION 1234, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES BS 1209 TO 1269, X= -27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,071 hrs · 23,777 cycles
SEAT TRACK AT STATION 1156, X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1156, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 1149 TO STATION 1209, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2024
Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 98,237 hrs · 23,254 cycles
ON TAKE OFF ENGINE 1 COMPRESSOR STALLED WITH N1 ROLL BACK X 3. NO OTHER INDICATIONS. DUMPED 130K AND RETURNED TO CDG. REPLACED #1 ENGINE HP FUEL PUMP PER MM 73-12-01-4-1. REMOVED AND REPLACED #1 ENG HMU IAW AMM 73-21-01-4-1. PERFORMED ENG #1 WET MOTOR TEST 01W AND ENG-UP LEAK TEST 10 IAW MM 71-00-00-5. PERFORMED ENG-UP LEAK CHECK TEST 10 AND ECU RETURN TO SERVICE. TESTED IAW MM 73-21-02-5-1 , NO LEAKS FOUND AND ALL TEST PASSED, IAW FIM 71-00 FAULT TREE, FIGURE 106. PERFORMED ENGINE NR 1 POWER ASSURANCE TEST (06) IAW MM TASK 71-00-00-700-804, ALL PARAMETERS NORMAL, ACFT OK FOR SERVICE.
2023
Part: SIGN — LOOSE (ZONE 200) · airframe 95,849 hrs · 22,539 cycles
LH EXIT SIGN PANEL COVER OUT OF POSITION. INSTALLED AND REPOSITIONED LH EXIT SIGN COVER.
Part: FRAME — CRACKED (300) · airframe 95,562 hrs · 22,465 cycles
DURING THE BANJO FITTING REPAIR OF THE FASTENERS REMOVAL ACCESS, ZONE 360 RIGHT HAND LOWER VERTICAL STABILIZER #364QR ACCESS PANEL SURROUNDING FRAME FOUND CRACKED, LOCATED BETWEEN STATION 2142 AND STATION 2164. RIGHT LOWER VERTICAL STABILIZER #364QR ACCESS PANEL SURROUNDING BETWEEN STATION 2142 AND STATION 2164 CRACKED FRAME REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01- 0G. FRAME FABRICATED AS PER DOUGLAS DRAWING #AJC 7593 REVISION Z. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100
Part: SPLICE — CRACKED (100) · airframe 95,562 hrs · 22,465 cycles
CENTER AVIONICS COMPARTMENT, COMPARTMENT RIGHT HAND SIDE SPLICE FITTING AT STATION 1139 APPROXIMATELY LONGERON 29 - LONGERON 30 FOUND CRACK. CENTER AVIONICS COMPARTMENT, COMPARTMENT RIGHT HAND SIDE CRACKED SPLICE FITTING AT STATION 1139 APPROXIMATELY LONGERON 29 - LONGERON 30 REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. FABRICATED (MACHINING) SPLICE FITTING AS PER DOUGLAS DRAWING AAA7042 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (N/A) · airframe 95,562 hrs · 22,465 cycles
LEFT HAND FIXED LEADING EDGE SLAT TRACK #8 CUTOUT OUTBOARD EDGE AT STATION XOS 551 SKIN CRACKED. REPAIR CARRIED OUT AS PER EA # 1-5720-T0373058 PART 1 TITLE:WING ÿ½ SECONDARY WING STRCT ÿ½ REPAIR FOR LEFT WING LEADING EDGE SKIN (P/N: ARB 2886-503). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
Part: SPLICE — CORRODED · airframe 95,562 hrs · 22,465 cycles
LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-62, LONGERON 48 RIGHT HAND SPLICE FITTING FOUND WITH COROSSION. LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-62, LONGERON 48 RIGHT HAND CORRODED SPLICE FITTING REMOVED AND REPLACED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING AEA7653 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: RIB — CRACKED · airframe 95,562 hrs · 22,465 cycles
LEFT HAND LEADING EDGE #3 SLAT INTERNAL RIB AT STATION XOS 505.972 FOUND CRACKED. LEFT HAND LEADING EDGE #3 SLAT INTERNAL AT STATION XOS 505.972 CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1676 REVISION E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: RIB — CRACKED · airframe 95,562 hrs · 22,465 cycles
LEFT HAND LEADING EDGE #3 SLAT INTERNAL RIB AT STATION XOS 511.337 FOUND CRACKED. LEFT HAND LEADING EDGE #3 SLAT INTERNAL AT STATION XOS 511.337 CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1677 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FRAME — CRACKED (300) · airframe 95,562 hrs · 22,465 cycles
EMPENNAGE: ZONE 360, LEFT HAND LOWER VERTICAL STABILIZER #363HL ACCESS PANEL SURROUNDING FRAME FOUND CRACKED, LOCATED BETWEEN STATION 2125 AND STATION 2137. EMPENNAGE: ZONE 360, LEFT HAND LOWER VERTICAL STABILIZER #363HL ACCESS PANEL BETWEEN STATION 2125 AND STATION 2137 CRACKED FRAME REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. FRAME FABRICATED AS PER DOUGLAS DRAWING #AJC 7593 REVISION Y. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Part: UNKNOWN — UNKNOWN (N/A) · airframe 95,562 hrs · 22,465 cycles
RIGHT HAND OUTBOARD FIXED LEADING EDGE AT STATION XOS 944 #15 SLAT TRACK CUTOUT INBOARD CORNER CRACKED.
Part: TRACK — CRACKED (200) · airframe 95,562 hrs · 22,465 cycles
LOWER CENTER CARGO COMPARTMENT STATION 1701, X-75 CEILING AREA SEAT TRACK FOUND WITH CRACK. LOWER CENTER CARGO COMPARTMENT CEILING AREA, CRACKED SEAT TRACK AT STATION 1701, X-75.25 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1711 TO EXISTING SPLICE STATION 1671, X= -47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — DAMAGED (200) · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1611, X = -8.50 CROWN AREA DAMAGED. CABIN ÿ½ AT SEAT TRACK STATION 1611, X = -8.5 DAMAGED CROWN AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1591 TO STATION 1651, X= -8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — CORRODED · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1149, X = -47.50 CORROSION. CABIN ÿ½ CORROSION AT SEAT TRACK STATION 1149, X = -47.5 EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1129, X=-47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — CHAFED (200) · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1671, X = -47.50 CROWN AREA CHAFFING MARKS. REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1691, X= -47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — DAMAGED (200) · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1540, X = 8.50 CROWN AREA DAMAGED. CROWN AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1571 TO STATION 5-123/1531, X= 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED · airframe 95,562 hrs · 22,465 cycles
RIGHT HAND OUTBOARD FIXED LEADING EDGE LOWER SKIN AT STATION XOS 990 FOUND CRACKED. RIGHT HAND OUTBOARD FIXED LEADING EDGE LOWER SKIN AT STATION XOS 990 FOUND CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-01-2R REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — DAMAGED · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1325, X = 8.50 CROWN AREA DAMAGED. CABIN ÿ½ AT SEAT TRACK STATION 1325, X = 8.5, CROWN DAMAGED AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1351 TO EXISTING SPLICE STATION 1311, X=8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — CORRODED · airframe 95,562 hrs · 22,465 cycles
CABIN - SEAT TRACK STATION 1405 TO 1436, X = -8.50 CORROSION. CABIN ÿ½ CORROSION AT SEAT TRACK STATION 1405 TO 1436, X = -8.5 EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1471 TO EXISTING SPLICE STATION 1391, X=-8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED · airframe 95,562 hrs · 22,465 cycles
LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRUNNION — CRACKED (110) · airframe 95,562 hrs · 22,465 cycles
DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.2ÿ½ AT STATION Y = 595. LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA AT STATION Y = 595 CRACK REPAIR CARRIED OUT AS PER MD-11 SRM 53-10-14-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100
Part: SPAR — CRACKED (300) · airframe 95,562 hrs · 22,465 cycles
WHILE ACCOMPLISHING RIGHT HAND NUMBER 4 BANJO FITTING INSPECTION AS PER WORK CARD T1-5530-49623C P4, LEFT HAND FORWARD LOWER SPAR RADIUS FOUND CRACK BETWEEN LOWEST TWO FASTENERS STATION Y = 2164. CRACK AT LEFT HAND FORWARD LOWER SPAR RADIUS BETWEEN LOWEST TWO FASTENERS STATION Y= 2164 REPAIRED PER E.A. #1-5530-T0373036 P1. TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LHS & RHS FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRUNNION — CRACKED (100) · airframe 95,562 hrs · 22,465 cycles
WHILE ACCOMPLISHING E.O.T1-5340-117249B-P4, FOUND RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING HAVE CRACKED AT STATION Y = 595. RIGHT HAND NOSE LANDING GEAR TRUNION FITTING AT STATION Y = 595 CRACKED REPAIR CARRIED OUT AS PER MD-11 SRM 53-10-14-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. REPETITIVE INSPECTION REQUIRMENT- INITIAL AT 1,500 CYCLES AND AT INTERVAL 1,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 53-10-14-2R TABLE 201 / REPAIR 2.
Part: UNKNOWN — CRACKED · airframe 95,562 hrs · 22,465 cycles
RIGHT HAND WING - OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 610 CLIP SUPPORT CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 610 CRACKED CLIP SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. CLIP SUPPORT FABRICATED AS PER DOUGLAS DRAWING ARB 2917 REVISION L. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRACK — CORRODED (200) · airframe 95,562 hrs · 22,465 cycles
CABIN ÿ½ SEAT TRACK STATION 6 - 35, X = - 47.50 CORROSION. EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 6-60 TO EXISTING SPLICE STATION 6-0, X= -47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED · airframe 95,562 hrs · 22,465 cycles
RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 612 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 612 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SPAR — CRACKED (300) · airframe 95,562 hrs · 22,465 cycles
DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP, FOUND 01 EACH CRACK WITH LENGTH APPROXIMATELY 0.4ÿ½ FROM 03RD FASTENERS BELOW ZEE CHANNEL STATION Y = 2164. 01 EACH CRACK WITH LENGTH APPROXIMATELY 0.4" FROM FASTENER BELOW ZEE CHANNEL STATION Y=2164 AT RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP, REPAIRED PER E.A. #1-5530-T0373036 P1. TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LHS & RHS FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: CONNECTOR — NOT SEATED (TRANSDUCER) · airframe 95,520 hrs · 22,454 cycles
NR 7 TIRE INITIALLY INDICATED A LEVEL 2 TIRE FAILURE DURING CRUISE AT FL370. THE CONFIG DISPLAYED A BLANK WHERE NR 7 IS INDICATED. THE CONFIG DISPLAY WOULD SUBSEQUENTLY SHOW LOW PRESSURE, THEN NORMAL PRESSURE, BUT WOULD CYCLE BACK TO NO DISPLAY. EMERGENCY DECLARED. ALL TIRE PRESSURES ARE REQD TO B E CHECKED BEFORE THE FIRST FLIGHT OF EACH DAY. CHECK FOUND NR 7 TIRE PRESSURE TRANSDUCER CONNECTOR NOT FULLY TIGHTEN, RETIGHTEN NR 7 TIRE PRESSURE TRANSDUCER CONNECTOR AND CHECK NORMAL IAW AMM 32-42-01-4, PRECAUTIONALY R & R BTMTP COMPUTER & RTS TEST NORMAL IAW AMM 32-46-02-4, ACFT OK FOR SERVICE. ORIG SUBMISSION DATE: 1/30/2023
Part: SENSOR — FAILED (BLEED SYSTEM) · airframe 95,436 hrs · 22,416 cycles
5 MINUTES AFTER ENGAGING WING & TAIL AI ON DEPARTURE WE RECEIVED A LEVEL 1 BLEED AIR 2 OFF. THE ALERT DISAPPEARED WHEN THE AI WAS TURNED OFF. WE PLACED THE ESC IN MANUAL AND REENGAGED THE AI. THE LEVEL 1 ALERT RETURNED AND WENT AWAY WHEN THE AI WAS TURNED OFF. AFTER SWITCHING CONTROLLERS IN AUTO WE REENGAGED THE AI. THE BLEED AIR TEMP INCREASED TO 270 DEGREES, TURNED RED AND THE SYTEM TURNED BLEED 2 OFF. WE TURNED THE AI OFF AND RETURNED TO MEMPHIS. REMOVED AND REPLACED D1-8251 (TI-2) AND REINSTALLED PSC-1. OPS CHECK GOOD. ORIGINAL SUBMISSION DATE: 1/13/2023
2022
Part: PIPE — NONE (N/A) · airframe 93,456 hrs · 21,853 cycles
LEVEL 2 HYD 1 FAIL DURING CLIMB OUT. HYDRAULIC 1 RESERVOIR QUANTITY INDICATED 0.0 ON THE HYDRAULIC SYNOPTIC. REPAIRED HYDRAULIC LINE USING RYNGLOK METHOD. REF MD-11 AMM 20-10-01-2. LEAK AND OPS CHECKS GOOD. REF WRI 57-30/2508 FOR PANEL CLOSE UP.
2021
Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
WHILE ACCOMPLISHING SPECIAL / NONROUTINE MAINTENANCE FORM # N01252 AFT CARGO COMPARTMENT RIGHT HAND STATION 1951 LONGERON 40 RIGHT FOUND CORRODED. AFT CARGO COMPARTMENT RIGHT HAND STATION 1946 TO STATION 2007 LONGERON 40 RIGHT RIGHT AREA REPAIRED AS PER SRM 53-00-05-2R FIGURE 202 AND FIGURE 201 REPAIR 1. REPAIR REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
WHILE ACCOMPLISHING SNRM #N00989 FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 999 TO STATION 1019 X = 27.5 CORROSION . MAIN DECK CARGO COMPARTMENT SEAT TRACK STATION 999 TO STATION 1019 , X = 27.5 , CORROSION FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 989 TO STATION 1029 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
WHILE ACCOMPLISHIMG SNRM : N01010 FOUND MAIN DECK CARGO SEAT TRACK AT STATION 1541 TO STATION 1561 X = 75.25 CORROSION . MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 TO STATION 1561 X = 75.25 CORROSION FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 5-123/1531 TO STATION 1571 X= 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: LONGERON — CRACKED (AFT CARGO) · airframe 91,049 hrs · 21,155 cycles
AFT CARGO COMPARTMENT STATION 1853 TO 1873 RIGHT HAND LONGERON 42 RIGHT FOUND CRACK. AFT CARGO COMPARTMENT STATION 1841 TO STATION 1893.15 RIGHT HAND LONGERON SPLICE SPLICE FITTING 42 RIGHT REMOVED AND REPLACED AS PER ENGINEERING AUTHORIZATION 1-5310- 1-5310-T0359289 P1 TITLE : FUSELAGE - MAINFRAME - AFT FUSELAGE - CRACK DAMAGES FOUND ON LONGERON L - 42R AT STA 1893.150 , AND LONGERON SPLICE FITTING BETWEEN STA 1852.55 AND STA 1861.05. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: LONGERON — CRACKED (AFT CARGO) · airframe 91,049 hrs · 21,155 cycles
WHILE ACCOMPLISHING SPECIAL / NONROUTINE MAINTENANCE FORM # N01336 FOUND AFT CARGO COMPARTMENT RIGHT HAND BETWEEN STATION 1887 TO STATION 1902 LONGERON #42 #42 RIGHT CRACK. AFT CARGO COMPARTMENT RIGHT HAND BETWEEN STATION 1887 TO STATION 1926.700 LONGERON 42 RIGHT REPAIRED AS PER ENGINEERING AUTHORIZATION : 1-5310-T0359289 P1 TITLE : FUSELAGE - MAINFRAME - AFT FUSELAGE - CRACK DAMAGES FOUND ON LONGERON L- 42R AT STA 1893.150, AND LONGERON SPLICE FITTING BETWEEN STA 1852.55 AND STA 1861.05. 1861.05. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1621 LEFT HAND X = 27.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT LEFT HAND SEAT TRACK STATION 1621 , X = 27.5 , CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1611 TO EXISTING SPLICE STATION 1671 , X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1741 TO STATION 1761 RIGHT HAND X = - 8.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1741 TO STATION 1761, X = - 8.5 CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1771 , X= - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1681 TO 1701 RIGHT HAND X = - 8.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1681 TO STATION 1701 X = - 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1771 X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REFER TO SNRM N01043 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1701 TO 1761 LEFT HAND X = 27.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT LEFT HAND SEAT TRACK STATION 1701 TO STATION 1761 , X = 27.5 CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION STATION 1671 TO EXISTING SPLICE STATION 1771 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1661 TO 1681 RIGHT HAND X = - 8.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1661 TO STATION 1681 , X = - 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1771 , X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REFER TO SNRM N01043 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1621 TO 1661 RIGHT HAND X = - 75.25 SEAT TRACK FOUND CORRODED . MAIN DECK AT SEAT TRACK RIGHT HAND STATION 1621 TO STATION 1661 , X = - 75.25 CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPLACEMENT FROM STATION 1591 TO STATION 1671 , X = - 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1601 TO STATION 1621 RIGHT HAND X = - 75.25 SEAT TRACK FOUND CORRODED . MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1601 TO STATION 1621 , X = - 75.25 CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPLACEMENT FROM STATION 1591 TO STATION 1671 , X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N01029 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: LONGERON — CORRODED (CENTER CARGO) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
CENTER CARGO COMPARTMENT STATION 1701 RIGHT HAND LONGERON 48 RIGHT FOUND CORRODED. CENTER CARGO COMPARTMENT STATION 1691 TO STATION 1707 RIGHT HAND LONGERON 48 RIGHT REPAIRED AS PER ENGINEERING AUTHORIZATION 1-5310-T0359099 P1 TITLE : FUSELAGE - MAINFRAME- AFT INTERMEDIATE FUSELAGE - LONGERON L - 48R SPLICE REPAIR AT AT STA 1691. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1581 TO 1621 LEFT HAND X = 75.25 SEAT TRACK FOUND CORRODED . MAIN DECK AT LEFT HAND SEAT TRACK STATION 1581 TO STATION 1621 , X = 75.25 CORROSION CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1571 TO STATION 1631 , X = 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
MAIN DECK STATION 1720 TO 1761 RIGHT HAND X = - 27.5 SEAT TRACK FOUND CORRODED . MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1720 TO STATION 1761 , X = - 27.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1711 TO STATION 1811 , X = -27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1761 TO STATION 1801 X = - 27.5 FOUND CORROSION . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1761 TO STATION 1801 X = - 27.5 CORROSION FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1711 TO STATION 1811 , X = - 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REFER TO SNRM N01042 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: LONGERON SPLICE — CRACKED (FWD CARGO) · airframe 91,049 hrs · 21,155 cycles
FORWARD CARGO COMPARTMENT STATION 1119 TO STATION 1139 RIGHT HAND LONGERON # 46 SPLICE FOUND CRACK. FORWARD CARGO COMPARTMENT STATION 1119 TO STATION 1139 RIGHT HAND LONGERON 46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. FABRICATED SPLICE AS PER DOUGLAS DRAWING ADA8424 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 91,049 hrs · 21,155 cycles
CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL # 232GF AT STATION 595 TO STATION 675 FOUND DELAMINATED. DELAMINATED FLOOR PANEL # 232GF AT CABIN STATION 595 TO STATION 675 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL # 232GF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FLOOR PANEL INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 91,049 hrs · 21,155 cycles
RIGHT HAND WING TRAILING EDGE - UPON REMOVAL OF INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE BUSHING FOUND BORE WITH CORROSION. CORROSION AT RIGHT HAND WING TRAILING EDGE - INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE ( HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA # 1-5750-T0330614 D PART 2 STEPS 1.F(1) AND 1.F(3). TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FORWARD HINGE (WING (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57500712 FOR WORK DETAILS.
Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 91,049 hrs · 21,155 cycles
LEFT HAND WING TRAILING EDGE - UPON REMOVAL OF INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE BUSHING FOUND BORE WITH CORROSION. CORROSION AT LEFT HAND WING TRAILING EDGE - INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE ( HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA # 1-5750-T0330613 D PART 2 STEPS 1.F. TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FORWARD HINGE (WING SIDE)- REPAIR- PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57500654 FOR WORK DETAILS.
Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 91,049 hrs · 21,155 cycles
AFT WASTE COMPARTMENT STATION 1974 TO 1985 RIGHT HAND LONGERON 43 RIGHT FOUND CORRODED. AFT WASTE COMPARTMENT STATION 1974 TO 1985 LONGERON 43 RIGHT CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CARRIED OUT REPAIR AS PER ENGINEERING AUTHORIZATION : 1-5310-T0359077 P1 TITLE : FUSELAGE - MAINFRAME - CORROSION REPAIR ON AFT FUSELAGE LONGERON 43R , BETWEEN BETWEEN STA1978 AND STA1981. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (LT WING LE) · airframe 91,049 hrs · 21,155 cycles
HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FIXED LEADING EDGE SKIN CORNER 11 ( FUEL ACCESS DOOR FORWARD INBOARD CORNER ) FOUND CRACK APPROXIMATE 0.3" AT XOS 610. CRACK AT LEFT HAND FIXED LEADING EDGE SKIN CORNER 11 AT XOS 610 ( FUEL ACCESS DOOR FORWARD INBOARD CORNER ) REPAIRED AS PER SRM 57-40-01-2R REPAIR 18 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT NEXT C CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION AT EVERY C CHECK NOT EXCEEDING 24 MONTHS AS PER SRM 57- 40-01-2R FIGURE 201 REPAIR 18 TABLE 204 REQUIREMENTS. METHOD BY VISUAL INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2020
Part: ROLLER TRAY — CORRODED (CENTER CARGO) · corrosion level 2 · airframe 90,176 hrs · 20,896 cycles
FUSELAGE-GENERAL-SPLICE REPAIR CARGO COMP ROLLER TRAY-REPAIR COMPLY WITH E.A. 1-5300-T0356398 REV NO. POS. P1, INFO 08SEP20 06:21. ATTACHED TO WORK ORDER 00078083, FACT 08SEP20 06:31, MEM U. COMPLIED WITH EA NR 1-5300-T0356398 PT1 SPLICE REPAIR CARGO COMP ROLLER TRAY. REF TO WORK ORDER 00078083. MINOR REPIAR TO SECONDARY STRUCTURE.
Part: TIRE — FAILED (MLG) · airframe 89,256 hrs · 20,678 cycles
AFTER CLEARING RUNWAY NBR 10 TIRE FAILURE ALERT APPEARED ASSOCIATED NOISE AND THUMP. DURING TAXI INTO GATE. FOUND NBR 10 M/W TIRE DAMAGED NO FURTHER DAMAGE FOUND. NBR 10 M/W TIRE ASSY REPLACED AS PER AMM 32-41-01-4 REV OCT 26/2018 .
Part: SWITCH — UNSECURE (MLG) · airframe 88,750 hrs · 20,530 cycles
PDIS 583 32-10 9710 14FEB20 IND OPEN AFTER DEPARTING KDTW AND SELECTING THE GEAR HANDLE UP, THE GEAR FAILED TO RETRACT WHICH WAS VERIFIED ON BOTH THE PRIMARY AND SECONDARY INDICATIONS. COMPLIED WITH QRH PROCEDURE WHICH RESULTED IN GEAR SAFELY DOWN/LOCKED, THEN WHEN DIRECTED TO RAISE THE GEAR AGAIN PER THE QRH, THE PRIMARY AND SECONDARY INDICATIONS SHOWED ALL 4 GEAR FAILED TO RETRACT. DIVERTED TO KIND REF FIM 32-30-01-01 AND WDM 32-63-01 PG 1 CHECKED GEAR HANDLE SWITCH S1-431 AND FOUND WIRE 2-20 DISCONNECTED FROM SWITCH. SO WE WILL CHANGE THE SWITCH PERFORMED MULTIPLE SUCCESSFUL GEAR SWINGS IAW MD11 AMM 32-31-00-5. PERFORMED PSEU FUNTIONAL TEST IAW MD11 AMM 31-71-01-2, TEST PASSES AND NO FAULTS IN PESU. OPS CHK NORMAL OK FOR SVC.
2019
Part: SUPPORT PLATE — LOOSE (L1 DOOR) · airframe 87,205 hrs · 19,997 cycles
L1 DOOR WILL NOT ARM. UPON INSPECTION, FOUND L1 DOOR AFT LOWER TORQUE TUBE SUPPORT PLATE LOOSE AND OUT OF ADJUSTMENT. ADJUSTED SERRATED PLATE AND ALL 16 STOP SCREWS FOR PROPER UNDERFAIR MEASUREMENT OF DOOR PER MD11 AMM 52-11-02-5 DOOR FUNCTION AND ARMING HANDLE OPS CHECK GOOD.
Part: CONNECTOR — SHORTED (EXTINGUISHER) · airframe 86,459 hrs · 19,769 cycles
PDIS 583 26-10 8406 02FEB19 CAN FACT U LOGPAGES:2905032 10 MIN AFTER TAKEOFF RECEIVED "ENG FIRE AGENT LO" ALERT.NO INDICATION LOW LIGHT ANY ENGINE ALERT BECOME INTERMITTENT IN DESCENT AND TAXI IN. FOUND "ENG FIRE AGENT LO" ALERT STILL SHOWING. SWITCHED DEU NO HELP. PER WDM 26-23-01 CHECKED WIRINGS AND FOUND CONNECTOR R5-1008A PIN 13A SHORT TO GROUND (1K OHM). IT'S ENG 1 AGENT 1 LOW PRESSURE. DISCONNECT #1 ENG AGENT 1 LOW PRESSURE SW CONNECTOR P1-1261. CHECKED LOW PRESSURE SW GOOD. AND CHECKED FOUND P1-1261 WIRE BROKEN AT THE PIN END. CHANGED THE PIN B PER SWPM. PER AMM 31-61-02-4,PERFORMED THE DEUS R-T-S TEST ALL NORMAL. AND PERFORMED FIRE WARNING TEST ALL NORMAL. MESSAGE CLEARED. A/C OK FOR SVC. SHGN 03FEB19 04:05 CAN U PER MD11 JRH RUN ALL 3 ENGS BY AMT 718486, AND ALL PARAMETERS NOMAL. FACT 03FEB19 04:08 CAN U CONSULT MOCC, A/C UP. A/C OK FOR SVC.
Part: CONNECTOR — BURNED (FUEL SSYTEM) · airframe 86,440 hrs · 19,762 cycles
REFUEL POWER LAMP DID NOT COME ON WHEN THE POWER SWITCH SET TO ARM POSITION & FOUND CB TRIPPED. CARRIED OUT TROUBLESHOOTING AS PER FIM 28-21-00 FOUND CONNECTOR P1-181 PINS BURNED. CONNECTOR P1-181 AND R5-181 REMOVED AND REPLACED AS PER SWPM 20-31-15 AND WDM 28-21-01, 28-22-05, 26-11-02, 34-43-01. CARRIED OUT LSDU OPERATIONAL TEST AS PER AMM 28-41-00-700-803 AND REFUEL CONTROL PANEL OPERATIONAL TEST AS PER AMM 28-41-95-4 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1867 X= -8.5 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 1867 X= -8.5 CORROSION AT FLANGE REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 1831 TO STATION 1887 X = -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
UPON REMOVAL FLOOR PANEL FOR TAIL TANK FUEL LINE CRACKED REPAIIR FOUND MAIN DECK FLOOR SEAT TRACK AT STA 1701 X = 75.25 CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK EXFOLIATION CORROSION AT STATION 1701 X= 75.25 CARRIED OUT SEAT TRACK REPAIR FROM STATION 1671 TO 1731 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X=-2 FOUND CRACKED AS MARKED. MAIN DECK AFT CRACKED FLOOR SUPPORT AT STATION 1887- STATION 2007 X= -2 REMOVED PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DWG AGA 7081 REV M. FABRICATED NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X=-25 FOUND CORROSION AS MARKED. MAIN DECK AFT FLOOR SUPPORT AT STATION 1887- 2007 X = -25 CORROSION REMOVED AND FOUND EXCEEDED LIMITED AS PER SRM 53-00-00-2R FIG 206 / REPAIR GENERAL. DAMAGED FLOOR SUPPORT REMOVED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DWG AGA 7087 REVISION M. NEW FABRICATED FLOOR SUPPORT INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FINGER DOUBLER — DETACHED (RT WING) · airframe 86,438 hrs · 19,761 cycles
RIGHT WING - TRAILING EDGE INBOARD ISLAND FIXED SKIN LOWER SURFACE FORWARD EDGE FINGER DOUBLER FROM XW 375 TO XW 399 FOUND DETACHED. REPAIR CARRIED OUT ON RIGHT WING - TRAILING EDGE INBOARD ISLAND FIXED SKIN LOWER SURFACE FROM STATION XW 375 TO XW 399 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1481 X= 27.5 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 1481 X = 27.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMGED1 FIGURE 101. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 AT STATION 1471 TO STATION 1491 X= 27.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX FOUND CRACKED AT STA 1305.250 - STA 1315.420, LONGERON 26 LEFT TO LONGERON 27 LEFT. MAIN DECK LEFT 3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.250 - STATION 1315.420 LONGERON 26 LEFT - LONGERON 27 LEFT CARRIED OUT REPAIR AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1311 X= 75.25 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 1311 X = 75.25 CORROSION REMOVED AND FOUND EXCEEDED LIMITED AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1261 TO STATION 1331 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
RADIOGRAPHY INSPECTION CARRIED OUT AND FOUND CRACK APPROX IMATELY 1" IN LENGTH AT STA 6-0 LONGERON 1 LEFT AT AFT CENTER SPLICE BETWEEN FASTENER 5 AND 6 AS MARKED. MAIN DECK CABIN AT STATION 6-0 LONGERON 1 LEFT AT AFT CENTRE CRACKED SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ADA 8413 REV B, FABRICATED NEW SPLICE PROTECTED AND PAINTED AS PER SRM 51-21-01-0G. NEW FABRICATED SPLICE INSTALLED PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (LE SLAT) · airframe 86,438 hrs · 19,761 cycles
LEFT WING - NUMBER 8 LEADING EDGE SLAT LOWER SURFACE SKIN FOUND CRACK ABOUT 2.7" LONG AT XOS 1178. REPAIR CARRIED OUT ON LEFT WING - NUMBER 8 LEADING EDGE SLAT LOWER SURFACE AT STATION XOS 1178 AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 3 AND ENGINEERING AUTHORIZATION 1-5750 -T0344706 P1 TITLE : WINGS -FLIGHT SURFACES - LT WING - NR 8 SLAT ASSY - INNER SKIN SRM SPLICE REPAIR AT STA XOS 1175.5 - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1159 X =-8.5 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 1159 X= -8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 1149 TO STATION 1209 X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 635 X= -8.5 FOUND CRACKED AS MARKED. MAIN DECK FLOOR CRACKED SEAT TRACK AT STATION 635 X = - 8.5 CARRIED OUT REPAIR AS PER STRUCTURE REPAIR MANUAL 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 705 X= -8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00510 FOR REPAIR DETAILS.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 695 X= -8.5 FOUND CRACKED AS MARKED. MAIN DECK FLOOR CRACKED SEAT TRACK AT STATION 695 X = -8.5 CARRIED OUT REPAIR AS PER STRUCTURE REPAIR MANUAL 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 705 X= -8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 755 X = 8.5 FOUND CROWN ELONGATED AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 755 X= 8.5 ELONGATED CROWN AREA CARRIED OUT REPAIR FROM STATION 745 TO 788 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 635 X = 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 635 X= 8.5 DAMAGED CROWN MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK CARRIED OUT REPAIR AT STATION 625 TO STATION 645 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 DAMAGED CROWN AREA MEASURED AND FOUND EXCEEDED LIMITED AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR AT STATION 1269 TO STATION 1311 X= 8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = -8.5 DAMAGED CROWN AREA REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 1259 TO STATION 1311 X = -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 86,438 hrs · 19,761 cycles
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT, CRACK INDICATION FOUND APPROXIMATELY 0.4" IN LENGTH AS MARKED AT CORNER NR 11 FUEL ACCESS DOOR AT FORWARD INBOARD CORNER AT XOS 610. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE SKIN AT CORNER NR 11 FUEL ACCESS DOOR AT STATION XOS 610 AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT NEXT "C" CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION AT EVERY "C" CHECK NOT EXCEEDING 24 MONTHS BY VISUAL INSPECTION METHOD AS PER SRM 57-40-01-2R TABLE 204 / REPAIR 18.
Part: DOUBLER — CRACKED (LT WING) · airframe 86,438 hrs · 19,761 cycles
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 632 FOUND CRACK. REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 632 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUESLAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 635 X = -27.5 FOUND CRACKED MAIN DECK FLOOR SEAT TRACK AT STATION 625 TO STATION 665 X=-27.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 86,438 hrs · 19,761 cycles
RIGHT WING - LEADING EDGE LOWER SURFACE FORWARD DOUBLER AT XOS 891 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING LEADING EDGE LOWER SURFACE FORWARD DOUBLER AT STATION XOS 891 AS PER SRM 57-40-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 86,438 hrs · 19,761 cycles
LEFT WING - FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK RIB DOUBLER ON LEFT WING - FIXED LEADING EDGE AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DOUBLER FABRICATED AS PER DRAWING ARB3954 REVISION K.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1531 X = - 47.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1531 X =-47.5 DAMAGED CROWN AREA MEASURED AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1551 X= -47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 86,438 hrs · 19,761 cycles
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 640 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 86,438 hrs · 19,761 cycles
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 785 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 785 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 770 X = 75.25 FOUND CROWN ELONGATED. MAIN DECK FLOOR SEAT TRACK AT STATION 770 X= 75.25 ELONGATED CROWN AREA CARRIED OUT REPAIR FROM STATION 769 TO 788 X= 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,438 hrs · 19,761 cycles
MAIN DECK FLOOR SEAT TRACK AT STATION 1531 X = 8.5 FOUND CROWN DAMAGED MAIIN DECK FLOOR SEAT TRACK AT STATION 1531 X= 8.5 DAMAGED CROWN MEASURED AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1551 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 86,438 hrs · 19,761 cycles
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 792 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2018
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,513 hrs · 19,132 cycles
DURING PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY LOW ALERT. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4, OPS TESTED OK & NO FAULT MESSAGE.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 84,287 hrs · 19,068 cycles
AFTER EMER LT. TEST: LVL 1 ALERT EMERGENCY LIGHT BATTERY LOW. REPLACEMENT OF EMERGENCY LIGHT BATTERY, OPS CHECKED GOOD.
2017
Part: BATTERY — FAULTED (EMERGENCY LIGHT) · airframe 83,711 hrs · 18,911 cycles
DURING PREFLIGHT, DURING AN EMERGENCY LIGHT TEST RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW DISPLAYED. PERFORMED AN OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. IAW AMM 33-51-01-5
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,726 hrs · 18,915 cycles
ON PREFLIGHT DURING EMERGENCY LIGHT TEST GOT "EMER LT BAT 1 LO" DISPLAYED. PERFORMED OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. REF AMM 33-51-01-5.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.316", FINAL HOLE DIA 2.320", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2B. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACHED INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331715 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT LOWER BOLT H0LE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIAMETER 0.406 INCH; FINAL HOLE DIAMETER 0.422 INCH; MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2C. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 0.405", FINAL HOLE DIA 0.422", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2C. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 1.281", FINAL HOLE DIA 1.285", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 20. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331716 PART 1 STEP 2C. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331719 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226" MAXIMUM ALLOWABLE HOLE DIA 1.220", OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750- T0331716 PART 1 STEP 2C. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331719 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 20. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331715 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.410", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.405". MINIMUM ALLOWABLE THICKNESS 0.408". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2A AND STEP 2. REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD LUG SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.380" MATERIAL REMOVED: 0.003" REMAINING THICKNESS: 0.377" MINIMUM ALLOWABLE THK: 0.380". REPAIR CARRIED OUT PER EA 1-5750-T0331715 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.402" , MATERIAL REMOVED 0.008", REMAINING THICKNESS 0.394". MINIMUM ALLOWABLE THICKNESS 0.408". LOWER MOUNT INBD AND OUTBD BORE SHOULDER BUSHING (2 EA) FABRICATED AND INSTALLED AS PER EA 1-5750-T0331716 PART 1 STEP 2A AND STEP 2. LOWER MOUNT OUTBD BORE SURFACE SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0331716 PART 1 STEP 2. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.405", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.400". MINIMUM ALLOWABLE THICKNESS 0.408". SHOULDER BUSHING MACHINING AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2A AND STEP 2. REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 1139, X=- 8.5 FOUND CORROSION AS MARKED. MAIN DECK CORRODED FLOOR SEAT TRACK AT STA 1139, X=- 8.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-100 TO STA 1149, X= - 8.5 AS PER SRM 53-00-02-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMMM 6-2-100. CORROSION ON SEAT TRACK EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 6-96, X=-8.5 FOUND CRACKED. MAIN DECK CRACKED FLOOR SEAT AT STA 6-96, X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 6-60 TO STA 6-100, X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 REMOVED PER AMM 53-21-10-2. NEW SUPPORT PANEL P/N: WSP0785-501 FABRICATED PER DWG WSP0785 REV B. NEW FLOOR SUPPORT PANEL INSTALLED PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= -27.5 TO X= -36 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 REMOVED AS PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0785 REV B, P/N: WSP0785-502, NEW FLOOR SUPPORT PANEL INSTALLED AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. FLOOR SUPPORT PANEL AT STA 488, X= 0.0 TO X= -8.5 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X=8.5 TO X= 19 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= 8.5 TO X= 19. REMOVED AS PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0786 REV B, P/N: WSP0786-501. NEW FLOOR SUPPORT PANEL INSTALLED AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= 8.5 TO X= 19 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 REMOVED PER AMM 53-21-10-2, NEW FLOOR SUPPORT PANEL P/N: WSP0790-502 FABRICATED PER DWG WSP0790 REV A. NEW FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 INSTALLED AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36. REMOVED AS PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0785 REV B P/N: WSP0785-502. NEW FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36 INSTALLED AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= 27.5 TO X= 36 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL PN: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 REMOVED PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0786 REV B AND NEW FLOOR SUPPORT PANEL PN: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 INSTALLED AS PER AMM 53-21- 10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= -17 TO X= -27.5 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=86.25 TO X= 107.25 CORROSION AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDED LIMIT AS PER SRM 53-20- 50 2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 REMOVED PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0785 REV B, P/N: WSP0785-501. NEW FLOOR SUPPORT PANEL INSTALLED PER AMM 53-21-10-2. REPAIR CLASSIFIED PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= -8.5 TO X= -17 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 REMOVED AS PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED PER DWG WSP0785 REV B, P/N: WSP0785-501. NEW FLOOR SUPPORT PANEL INSTALLED AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= 0.0 TO X= 8.5 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
UPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5. REMOVED AS PER AMM 53-21-10-2. NEW FLOOR SUPPORT PANEL FABRICATED AS PER DWG WSP0785 REV B, P/N: WSP0785-501. NEW FLOOR SUPPORT PANEL P/N: WSP0785-501 INSTALLED AT STA 488, X= 19 TO X= 27.5 PER AMM 53-21-10-2. CORROSION ON FLOOR SUPPORT PANEL AT STA 488, X= 19 TO X= 27.5 EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=-36 TO X=-47.5 CORRODED AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDED LIMIT AS PER SRM 53-20-50-2R FIG 201 REPAIR 1.
Part: SKIN — CRACKED (LT WING) · airframe 82,122 hrs · 18,410 cycles
DURING ACCOMPLISHMENT OF NDT INSPECTION AT LT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT AT STA XORS=696, 01 EA FASTENER HOLE 32 FOUND CRACK AS MARKED. LT WING LOWER SKIN PANEL ACCESS DOOR CUT OUT AT STA XORS 696, 01 EACH CRACKED FASTENER HOLE CARRIED OUT BUSHING REPAIR AS PER SRM 57-20-02-2R FIG 2014 REPAIR 5. THE REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
DURING ACCOMPLISHMENT OF NDT INSPECTION AT RT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT AT STA XORS=696, 01 EA FASTENER HOLE 18 FOUND CRACK AS MARKED. RT WING LOWER SKIN PANEL ACCESS DOOR CUTOUT AT STA XORS, 01 EACH CRACKED FASTENER HOLE CARRIED OUT BUSHING REPAIR AS PER SRM 57-20-02-2R FIG 201 REPAIR 5. THE REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
WHILE REMOVING MAIN DECK R3 DOOR FOR ACCESS FOUND R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO STA 1315.42 CRACKED AS MARKED. MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO STA 1315.42 REPAIRED AS PER EA 1-5310-T0331819 PT 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING LEADING EDGE COMPARTMENT XOS 695 BEADED DOUBLER CRACKED. CARRIED OUT INNER DOUBLER REPAIR AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1688, X= 8.5 FOUND CORROSION MAIN DECK CORRODED FLOOR SEAT TRACK AT STA 1688, X= 8.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1670 TO STA 1751, X= 8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON SEAT TRACK AT STA 1688, X= 8.5 EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
Part: DOUBLER — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING LEADING EDGE COMPARTMENT XOS 645 BEADED DOUBLER CRACKED. CARRIED OUT INNER DOUBLER REPAIR AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING NR 12 SLAT TRACK DOOR CUTOUT CRACKED. RT WING NR 12 SLAT TRACK DOOR CUT OUT CRACKED SKIN CARRIED OUT DOUBLER REPAIR AS PER EA NR 1-5730-T0331817 PT1. THE REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. REFER TO WRI 57305212 EA NR 1-5730-T0331817 PT 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1282 X= 47.5 FOUND CROWN DAMAGED AS MARKED. MAIN DECK DAMAGED FLOOR SEAT TRACK AT STA 1282, X= 47.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1246 TO STA 1311, X= 47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. GOUGE MARK ON SEAT TRACK AT STA 1282 X= 47.5 EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 755, X=-8.5 FOUND CROWN DAMAGED. MAIN DECK DAMAGED SEAT TRACK AT STA 755, X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 745 TO STA 785, X=-8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. GOUGES MARK ON SEAT TRACK AT STA 755, X= -8.5 FOUND EXCEED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: SKIN — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING SLAT DRIVE MECHANISM ACCESS DOOR CUTOUT I/B FORWARD CORNER CRACKED. RT WING SLAT DRIVE MECHANISM ACCESS DOOR CUTOUT INBOARD FORWARD CORNER CRACKED AREA CARRIED OUT DOUBLER REPAIR AS PER SRM 57-40-01-2R FIG 201 REPAIR 17. THE REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: RIB — CRACKED (LT WING) · airframe 82,122 hrs · 18,410 cycles
LT WING L/E COMPARTMENT XOS 906 FIXED L/E RIB DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. THE NEW RIB DOUBLER FABRICATED AS PER DRAWING: ARB1249 REV "AA". THE REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 5-113 X=-27.5 FOUND CROWN DAMAGED. MAIN DECK DAMAGED FLOOR SEAT AT STA 5-113 X=-27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-83 TO STA 5-123, X=-27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. GOUGES MARK AT FLOOR SEAT TRACK AT STA 5-113 X=-27.5 FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1561 X=-8.5 FOUND CORROSION. MAIN DECK CORRODED FLOOR SEAT AT STA 1561 X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-123 TO STA 1590, X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION AT FLOOR SEAT TRACK AT STA 1561 X=-8.5 FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
RT OVERWING LANDING GEAR FITTING DOUBLER FOUND CORROSION AT XOS 264. RT OVERWING LANDING GEAR FITTING DOUBLER CORRODED AREA CARRIED OUT REPAIR AS PER EA 1-5730-T0331654 PART 1. WINGS-PLATES AND SKINS- RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN S-1 AND REAR SPAR FOR WORK DETAILS. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.
Part: RIB — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING L/E COMPARTMENT XOS 643 RIB FORMER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. THE NEW RIB FORMER FABRICATED AS PER DWG ARB2917 REV L. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1845 X= 8.5 FOUND CORROSION. MAIN DECK CORRODED FLOOR SEAT AT STA 1845 X= 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1751 TO STA 1887, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION AT FLOOR SEAT TRACK AT STA 1845 X= 8.5 FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: RIB — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING L/E COMPARTMENT XOS 585 RIB FORMER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. THE NEW RIB FORMER FABRICATED AS PER DWG ARB2931 REV H. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: STRINGER — CRACKED (RT WING) · airframe 82,122 hrs · 18,410 cycles
RT WING L/E COMPARTMENT XOS666 STRINGER CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 755 , X= 47.5 FOUND CROWN DAMAGED. MAIN DECK DAMAGED FLOOR SEAT TRACK AT STA 755, X= 47.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 725 TO STA 765, X= 47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. GOUGE MARK ON SEAT TRACK CROWN AREA AT STA 755, X= 47.5 EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1470, X=-75.25 FOUND CROWN DAMAGED. MAIN DECK DAMAGED FLOOR SEAT TRACK AT STA 1470, X=-75.25 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1451 TO STA 5-0 , X=-75.25 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. GOUGE MARK ON SEAT TRACK AT STA 1470, X=-75.25 EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1781 X= 8.5 FOUND CORROSION AS MARKED. MAIN DECK CORRODED FLOOR SEAT AT STA 1781 X= 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1751 TO STA 1887, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION AT FLOOR SEAT TRACK AT STA 1781 X= 8.5 FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,122 hrs · 18,410 cycles
MAIN DECK FLOOR SEAT TRACK AT STA 1810 X= 27.5 FOUND CORROSION. MAIN DECK CORRODED FLOOR SEAT AT STA 1810 X= 27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1771 TO STA 1887, X= 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION AT FLOOR SEAT TRACK AT STA 1810 X= 27.5 FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 82,122 hrs · 18,410 cycles
CENTER LANDING GEAR WHEEL WELL RT FORWARD T-CHORD FOUND CRACKED AS MARKED, STA X CW 31.500 CENTER LANDING GEAR WHEEL WELL RT FORWARD CRACKED T-CHORD REMOVED AND NEW T-CHORD INSTALLED AS PER SRM 51-31-01-0G, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
2016
Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 81,544 hrs · 18,212 cycles
L1 DOOR WON'T CLOSE. GETS TO BOTTOM OF TRAVEL AND STARTS TO COME BACK UP. FOUND L1 DOOR EXTERIOR DOOR SWITCH STICKING. REMOVED AND REPLACED THE SWITCH S1-1013 IAW WDM 52-11-01 AND OPS CHECKED GOOD IAW AMM 52-10-01-2.
Part: DOOR — MALFUNCTIONED (CABIN) · airframe 81,503 hrs · 18,196 cycles
L1 DOOR WILL NOT CLOSE ELECTRICALLY FORM INSIDE. CLOSE SWITCH, WILL CLOSE FROM OUTSIDE SWITCH. DUPLICATED THE PROBLEM WHEN USE INTERIOR CONTROL SWITCH TO CLOSE THE DOOR , THE DOOR AUTOMATICALLY REVERSERS DIRECTION TO UP WHEN SWITCH RELEASED TO CENTER POSITION. EXTERIOR SWITCH WORKING NORMAL. THE PROBLEM WAS FOUND TO BE INTERMITTENT.
Part: SOLENOID — FAILED (PAX DOOR) · airframe 81,473 hrs · 18,186 cycles
UNABLE TO CLOSE LEFT FWD ENTRY DOOR. WHEN IT GETS TO THE BOTTOM OF TRAVEL. IT AUTOMATICALLY REVERSES DIRECTION, THEN SELECTING DOWN ON THE DOOR SWITCH, CAUSES THE DOOR TO GO UP. OPERATED DOOR SEVERAL TIMES FROM INSIDE AND OUTSIDE, NOTICED DOOR LOCK PIN RELEASE SOLENOID STAYING ENGAGED AND A CONTINUITY CHECK OF THE TERMINALS SHOWED INTERMITTENT CONTACT BETWEEN A1 AND A2. REMOVED AND REPLACED FORWARD PAX DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06-4.
Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 81,376 hrs · 18,151 cycles
L1 DOOR WILL NOT STAY CLOSED OPENED AND CLOSED L1 DOOR IAW AMM 52-11-02-02. OPS CHECK GOOD FOR CONTINUED USE AT THIS TIME.
Part: BATTERY PACK — INOPERATIVE (R1 DOOR SLIDE) · airframe 81,130 hrs · 18,074 cycles
DURING PREFLIGHT, PUSH TO TEST LIGHT FOR THE R1 DOOR SLIDE WOULD NOT TEST. INSTALLED BATTERIES AND OPS CHECKED NORMAL IAW SMP.
Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 80,624 hrs · 17,880 cycles
R1 DOOR PRESS TO TEST SWITCH INOPERATIVE. REPLACED R-1 DOOR PRESS TO TEST SWITCH BATTERIES. OPS CK GOOD.
Part: SKIN — CRACKED (RT WING) · airframe 80,345 hrs · 17,786 cycles
ON WALK AROUND, FOUND RT WING LE CRACK, APPROX 3.5" AT INBD SIDE OF NR 6 SLAT. REPAIRED IAW EA 1-5730-T0325373 PART 1 & 2.
Part: SKIN — CRACKED (RT WING) · airframe 80,343 hrs · 17,785 cycles
ON WALK AROUND FOUND RT WING LE CRACK, APPROX 3.5" AT INBD SIDE OF NBR 6 SLAT. COMPLIED WITH STEPS 2 & 3 OF EA 1-5730-T0325373 PART 1 & STEP 10 OF EA 1-5730-T0325373 PART 2. ALL STEPS ON EA 1-5730-T0325373 PART 1 & PART 2 COMPLETE. OK FOR SERVICE.
Part: ACTUATOR — INOPERATIVE (L1 DOOR) · airframe 80,288 hrs · 17,768 cycles
L1 WILL NOT CLOSE ELECTRICALLY. MEL 52-10-01 CATEGORY C EXPIRATION 13 MAY16. L1 ELEC DOOR ACTUATOR INOPERATIVE. FOR EMER EGRESS, USE PNEUMATIC SYS TO OPEN DOOR.
Part: RELAY — FAILED (ENTRY DOOR) · airframe 80,071 hrs · 17,714 cycles
LEFT ENTRY DOOR INOPERATIVE FROM INSIDE SWITCH. OPERATIONS CHECKED DOOR BEFORE WORK BEGAN, DOOR OPERATIONS CHECKED GOOD. R & R RELAY R2-177. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 79,989 hrs · 17,689 cycles
L1 DOOR SHOWS OPEN ON STATUS PAGE WHEN CLOSED & SLIDE ARMED. CLEARED DEBRIS FROM GIRT BAR AREA. OPERATIONS CHECKED IAW MM 52-11-02-2. OK FOR SERVICE.
Part: CONTROL PANEL — LOOSE (L1 DOOR) · airframe 79,978 hrs · 17,684 cycles
UNABLE TO CLOSE DOOR L1. ON ARRIVAL DOOR OPERATED NORMALLY. FOUND INTERIOR CONTROL PANEL LOOSE. OPENED CONTROL PANEL & INSPECTED. NO DEFECTS OR DAMAGE NOTED. SECURED PANEL & OPERATIONS CHECKED NORMAL.
2015
Part: POWER SUPPLY — FAILED (CABIN) · airframe 788 hrs · 17,344 cycles
EMERGENCY LIGHT TEST GOT LOW BATTERY WARNING. R & R LIGHT POWER SUPPLY.
Part: SWITCH — INTERMITTENT · airframe 787 hrs · 17,325 cycles
DURING PREFIGHT CHECK FOUND EMER LIGHT TEST INTERMITTENT. FOUND TEST SWITCH S1-402 INTERMITTENT. R & R SWITCH S1-402. EMER LIGHTS TESTED OK.
Part: LIGHT — NONE (CABIN) · airframe 787 hrs · 17,324 cycles
EMERGENCY LIGHT TEST FAILED. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW MM 33-52-01-05. TEST PASSED.
Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 782 hrs · 17,158 cycles
AFTER TAKEOFF CENTER GEAR SHOWED UNSAFE UP. CONFIGURATION PAGE SHOWED CENTER GEAR UP. SLOWED TO 200 KTS, CYCLED GEAR OK WENT UP SAFE CONTINUED. REPLACED PRIMARY CLG LOCKED PROXIMITY SENSOR.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 782 hrs · 17,158 cycles
AFTER TAKEOFF CENTER GEAR SHOWED UNSAFE UP. CONFIGURATION PAGE SHOWED CENTER GEAR UP, SLOWED TO 200 KTS, CYCLED GEAR OK WENT UP SAFE CONTINUED.
Part: SKIN — CRACKED (FUELAGE) · airframe 782 hrs · 17,145 cycles
SUSPECTED CRACK AT THE RIGHT PACK BAY ACCESS DOOR, UPPER AFT, FUSELAGE SKIN CUT OUT. INSPECTED SUSPECT CRACK AREA IAW NTM 51-60-00. VERIFIED CRACK RUNNING FROM AFT CORNER OF CUT OUT, RUNNING AT APPROXIMATELY A 45 DEGREE UP & AFT. CRACK EXTENDS THROUGH THE FIRST RIVET & APPROXIMATELY 1/4" BEFORE THE NEXT RIVET. CUT OUT CRACK AT UPPER AFT CORNER OF DOOR CUT OUT WITH A .5 RADIUS IAW SRM 53-20-15-2R FIG 201. PERFORMED HFEC OF CUT OUT AREA IAW NTM PT 6. NO CRACKS NOTED. OK TO INSTALL REPAIR. COMPLIED WITH EA 1-5310-T0318974. FUSELAGE MAINFRAME NR 3 PACK DOOR JAMB, CRACK REPAIRED.
Part: TRANSMITTER — CRACKED (OIL SYSTEM) · airframe 774 hrs · 16,916 cycles
APPROX 1 HR INTO FLIGHT AT FL290, NOTICED NR 3 ENG OIL QTY INDICATING 0. INITIALLY OIL PRESS & TEMP MATCHED THE OTHER TWO ENGS. OVER NEXT 45 MINUTES, OIL PRESS DROPPED TO 15 PSI, PERFORMED PRECAUTIONARY SHUTDOWN. INSPECTED NR 3 ENG, LOWER HALF OF THRUST REVERSER COWLING IS WET. OPENED FAN COWL & THRUST REVERSER COWL IAW AMM71-10-00-2 FOUND OIL PRESS TRANSMITTER HAS CRACK. REPLACED NR 3 ENG OIL TRANSMITTER IAW MM 79-33-01-4-1 & SERVICED ENG OIL FOR PROPER LEVEL IAW MM 12-12-01-3-1. RAN NR 3 ENG & COMPLIED WITH WIND MILLING INSPECTION IAW MM 71-00-00-5-1 & ALSO 80% N2 ABOUT 5 MINUTES, FOUND NO OIL LEAK FROM AROUND OF OIL TRANSMITTER IAW JRH. ACFT OK FOR SERVICE.
Part: STOP FITTING — CRACKED (L3 DOOR) · airframe 774 hrs · 16,904 cycles
L3 CABIN DOOR HAS 2 EACH BROKEN STOP BRACKETS & 3 OTHER BRACKETS ARE CRACKED. R & R L3 DOOR IAW AMM 52-12-12-4.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
MAIN CABIN, SEAT TRACK IS DAMAGED AT STATION 1165, RBL 8. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 3.
Part: FITTING — CRACKED (THRUST REVERSER) · airframe 774 hrs · 16,904 cycles
1 INCH CRACK FROM RIVET TO RIVET ON NR 2 ENG LT THRUST REVERSER COWL. REPAIRED DISCREPANT CRACK IAW EA 1-7830-T0316190.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
MAIN CABIN, SEAT TRACK IS DAMAGED AT STATION 1406, RBL 8. REPAIRED MAIN DECK SEAT TRACK IAW SRM 53-00-52 REPAIR 3.
Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 774 hrs · 16,904 cycles
NUMBER 2 ENG RT FAN COWL, FWD LOWER JAMB AREA GOUGED. SKIN REPAIR IAW SRM 54-20-15 FIG 201 REPAIR 1.
Part: SKIN — CORRODED (FUEL TANK) · airframe 774 hrs · 16,904 cycles
UPPER CARGO COMPARTMENT UNDER FLOOR AREA CORROSION ON CTR WING BOX UPPER SURFACE. STATION 1159 LBL 12. ADDITIONAL CORROSION DOCUMENTED ON VARIOUS NR'S FOR THE SAME CTR WING TANK SKIN. N00445, N00446, N00447, N00448 ALL REPAIRED UNDER SAME EA. REMOVED CORROSION FROM CTR WING BOX UPPER SURFACE AT STATION 1159 LBL12 IAW SRM 51-21-01 & EA 5710-T0316075.
Part: ANGLE — DAMAGED (NR 2 COWLING) · airframe 774 hrs · 16,904 cycles
NUMBER 2 ENG RT FAN COWL LAND AREA, HAS TRIMMED L ANGLE. REPAIRED L ANGLE IAW SRM 51-35-01.
Part: SKIN — CRACKED (LT WING) · airframe 774 hrs · 16,904 cycles
LEFT WING DROOP LE TOP SURFACE APPEARS TO HAVE 2 SKIN CRACKS LOCATED AT TE INBD SIDE COMING FROM SCREW HOLE. REPAIR DOUBLER IAW SRM 57-40-01-2R FIG 201.
Part: SKIN — CRACKED (RT WING) · airframe 774 hrs · 16,904 cycles
RIGHT DLE, UPPER SURFACE HAS A CRACK MIGRATING FROM BOLT HOLE. REPAIR DOUBLER IAW SRM 57-40-01 FIG 201 REPAIR 5.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
MAIN CARGO, AFT LT STATION 1973 LBL 76, SEAT TRACK FLOOR SUPPORT LOBE HAS CORROSION. MARKED REPAIR SEAT TRACK IAW SRM 53-00-52-2R.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
MAIN DECK, AFT LT STATION 1911 AT LBL 54 TO LBL 87, FLOOR SUPPORT HAS CORROSION. R & R NEW FLOOR SUPPORT IAW DWG AGA7079.
Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
CENTER WW RT KEEL WEB STATION 1431 - 1441, Z=-90.00 OIL CANNING CONDITION IS BEYOND ALLOWABLE LIMIT, .190 IAW SRM 53-40-12-2R. DEFLECTION DEPTH IS .300. REPAIR IAW EA 1-5310-T0315766.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 774 hrs · 16,904 cycles
AFT RT EXTERIOR FUSELAGE, STATION 1980 FILLET SUPPORT STRUCTURE AJC7405 HAS 1 INCH CRACK EMANATING THROUGH RIVET. REPAIRED IAW SRM 53--00-00-2R.
Part: SKIN — DAMAGED (RT STRUT DOOR) · airframe 774 hrs · 16,904 cycles
RIGHT MLG STRUT DOOR HAS A TWO INCH LONG HOLE IN THE OUTER SKIN. REPAIR DAMAGE IAW SRM 51-71-00. PREP & PAINT IAW SRM 51-21-02.
2014
Part: SKIN — CRACKED (ZONE 600) · airframe 75,496 hrs · 16,297 cycles
CRACK ON RT WING LOWER SURFACE BETWEEN 6 & 7 SLATS. CONFIRMED END OF CRACK IAW NDTSPM PT 6. REMOVED CRACK IAW SRM 57-40-02 FIG 201. PERFORMED HFEC OF CUT OUT AREA. IAW NTSPM 06-10-01 010, NO DEFECTS NOTED. REPAIRED IAW SRM 57-40-02 REPAIR 7.
Part: COMPUTER — MALFUNCTIONED (NR 1) · airframe 74,760 hrs · 16,057 cycles
DURING GO AROUND FROM RUNWAY 8L, AFTER FLAG ELECTED TO 28, ACFT ACCELERATED TO APPROX 230 WHILE ON AUTO FLIGHT. FCP HAS BEEN SET TO 4000 FEET & ACFT FAILED TO LEVEL OFF AT ALTITUDE. FIRST OFFICER AS PF DISCONNECTED AUTO PILOT & ATTEMPTED TO RETURN ACFT TO SELECTED ALTITUDE. AUTO PILOT WAS REENGAGED, AIRPLANE REPEATED ITS CLIMB ABOUT FCP ELECTED ATTITUDE. AFTER REGAINING CONTROL & REINIT ARRIVAL AIRPORT & BUILDING APPROACH FOR PHNL 08L, FIRST OFFICER REPORTED THAT WITH SLATS EXTENDED & ZERO FLAP, AIRSPEED HOLLOW BUG INDICATED FLAP 35 SPEED. SECOND APPROACH AFTER FLAPS EXTENDED & COUPLED IN LAND WAS UNEVENTFUL. INTERROGATED CFDS FCC1 & FCC2, BOTH SHOWED NO FAULTS & NO 30 DAY HISTORY. PERFORMED AFS RTS TEST ON BOTH FCC1 & FCC2 IAW MM 22-01-10-5, ALL TESTS PASSED, ACFT OK FOR SERVICE.
2013
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,451 hrs · 15,963 cycles
DURING PREFLIGHT LEVEL LOW EMERGENCY LIGHT 1 LOW DISPLAYED DURING TEST. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-4. ADJUSTMENT TEST CHECKED OK PER AMM 33-51-01-5.
Part: FAIRING — DAMAGED (ZONE 400) · airframe 74,207 hrs · 15,868 cycles
FOUND NR 3 ENGINE PYLON AFT BOAT TAIL DAMAGED. FWD LOWER SECTION DEPARTED ACFT. DAMAGE TO AFT CENTER BODY AND TAIL CONE. DAMAGE TO EXHAUST NOZZEL AROUND TAIL CONE AT 12 O`CLOCK POSTION.
Part: PAINT — PEELING (RT AILERON) · airframe 72,911 hrs · 15,445 cycles
RT OTBD AILERON UPPER AND LOWER SURFACES PAINT PEELED. SURFACE PAINT TOUCHED UP IAW SRM 51-21-02, REV 52. REPAIR CLASSIFIED AS MINOR IAW GMM -6-2-100, REV 116.
Part: SKIN — CRACKED (ZONE 500) · airframe 72,911 hrs · 15,445 cycles
THREE FASTENER HOLES, NR 6, 8, 10 FOUND TO HAVE A CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 - 713.6. REPAIRED IAW SRM 57-20-02. REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,911 hrs · 15,445 cycles
DURING LOWER AFT CARGO COMPARTMENT CEILING INSPECTION, FOUND CABIN FLOOR SUPPORT WITH CORROSION AT BS 1887, X= -75. FLOOR SUPPORT REMOVED IAW AMM 20-50-02, REV 75.2. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551, REVISION G. NEW FLOOR SUPPORT INSTALLED IAW AMM 20-50-02, REV 75.2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,911 hrs · 15,445 cycles
DURING LOWER AFT CARGO BAY CEILING INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 1975, X= -107. SEAT TRACK BS 1897 -2007, R & R IAW SRM 53-00-52, REPAIR 6, REV 52 AND SRM 51-31-01 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,911 hrs · 15,445 cycles
DURING REMOVAL OF FLOOR PANEL FOR ACCESS. FOUND BS 1880, X= 47.25 SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52. REPAIR 1, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
Part: SKIN — CRACKED (ZONE 600) · airframe 72,911 hrs · 15,445 cycles
FIVE FASTENER HOLES, NR 8, 10, 13, 29, 32 FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 -713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
Part: STRUCTURE — DELAMINATED (LT ELEVATOR) · airframe 72,911 hrs · 15,445 cycles
DURING WALK AROUND, LT DETACHABLE ELEVATOR INBD EDGE FOUND DELAMINATED. DETACHABLE ELEVATOR ASSY R & R IAW AMM 21-30-10, REV 75.2. CARRIED OUT ELEVATOR RANGE OF MOVEMENT TEST IAW AMM 27-30-00-710-802 REV 75.2 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.
2012
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 71,105 hrs · 14,934 cycles
EMERGENCY LIGHT TEST FAILED & RECEIVED AN EMERGENCY LIGHTT BATTERY 6 LOW ALERT. R & R POWER SUPPLY IAW MM 33-51-01 AND TESTED OK.
Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,394 hrs · 14,741 cycles
STRUCTURE IN PACK BAY NR1 FOUND CORROSION AT STRINGER 18 AND 19. REPAIRED IAW SRM 53-00-05 REPAIR 2 FIGURE 201 AND DWG3353 SH1.
Part: HINGE FITTING — CORRODED (CARGO DOOR) · airframe 69,595 hrs · 14,543 cycles
MAIN CARGO DOOR UPPER HINGE FITTING RUSTED UNDERNEATH FOAM INSULATION IN SEVERAL AREAS. REPAIR OR REPLACE.
2011
Part: PANEL — DEPARTED (NR 3 NACELLE) · airframe 69,006 hrs · 14,409 cycles
ON ARRIVAL, FOUND ON INBD SIDE PYLON ENG 3, ON PANEL MISSING, AND SCRATCHED THE RT INBD FLAP. INSTALLED NR 3 ENGINE INBD SIDE PYLON ACCESS PANEL AS PER MM 70-00-00-0-1.
Part: FUEL TANK — CORRODED (BS 1251) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA1251 X=-107. ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1251 X= -107, CORRODED AREA REPAIRED IAW EA1-5710-143599. TITLE: WINGS -CTR WING UPPER SKIN SURFACE CORROSION - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 68,116 hrs · 14,185 cycles
LT WING OTBD AILERON LOWER SURFACE INBD EDGE FOUND DELAMINATED. COMPLIED WITH EA 1-5750-150345. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON CTR O/W FUEL CELL UPPER SURFACE AT STA 1229 X8 TO 27.5. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1242 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON THE CTR O/W FUEL TANK UPPER SURFACE AT STA 1236 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1244 X=-107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1229 X=8 TO -8. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1249 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRUCTURE — CORRODED (FUEL CELL) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1229, 47.5. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: STRINGER — CRACKED (ZONE 200) · airframe 68,116 hrs · 14,185 cycles
DURING X-RAY INSP, CRACK FOUND AT STA 5-0, STR 11L ON FWD INBD ROW NR3 TO NR4 FASTENER TO EDGE OF STRINGER AS MARKED. REPAIRED AS PER SRM 53-00-05 FIG 202 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: SEAT TRACK — CORRODED (BS 1139-1159) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK- CORROSION ON SEAT TRACK FLANGE AT BS 1139-1159 X=47.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1129 TO 1189 X=47.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: SEAT TRACK — CORRODED (BS 1239-1263) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK- CORROSION ON SEAT TRACK FLANGE AT STA 1239-1263 X=75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA1129 TO 1209 X= 75 AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV. 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 112.
Part: SEAT TRACK — CORRODED (BS 1179-1219) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
CORROSION ON SEAT TRACK FLANGE AT STA1179-1219 X=75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1129 TO STA.1269 X=75 AS PER SRM 53-00-52 FIG.201 REPAIR 1 REV.46. REFER TO SNRM N00637 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.112
Part: SEAT TRACK — CORRODED (BS 1239-1259) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
CORROSION ON SEAT TRACK FLANGE AT STA1239-1259 X=-8. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REFER TO SNRM N00739 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: SEAT TRACK — CORRODED (BS 1273-1289) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
CORROSION ON SEAT TRACK FLANGE AT STA1273-1289 X=-8. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV.46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: DOUBLER — CRACKED (LT MLG WW) · airframe 68,116 hrs · 14,185 cycles
CENTER LANDING GEAR WHEEL WELL - LT KEEL WEB- CUT-OUT DOUBLER (AILERON INPUT ROD) - FOUND CRACKED. CENTER LANDING GEAR WHEEL WELL LH KEEL WEB CUTOUT CRACK DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 REV 46. NEW DOUBLER FABRICATED AS PER DWG AEA0526 REV NC. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: PAN — CRACKED (MLG DOOR) · airframe 68,116 hrs · 14,185 cycles
RT MLG DOOR - FWD INBD CORNER (PAN) - FOUND CRACKED. REMOVED AND NEW CORNER INSTALLED AS PER SRM 51-31-01 REV 46. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: SEAT TRACK — CORRODED (BS 1219-1239) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON SEAT TRACK FLANGE AT STA 1219 - 1239 X= -27.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1209 TO 1269 X= -27.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV.46 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 112.
Part: SEAT TRACK — CORRODED (BS 1159) · corrosion level 2 · airframe 68,116 hrs · 14,185 cycles
MAIN DECK CORROSION ON SEAT TRACK FLANGE AT STA 1159 X=27.5. CORRODED SEAT TRACK AT STA. 1159 X=27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1129 TO STA.1169 X=27.5 AS PER SRM 53-00-52 FIG.201 REPAIR 1 REV. 46 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: CABLE — WORN (PAX DOOR) · airframe 67,072 hrs · 13,938 cycles
WHILE PERFORMING AFT DOOR CHECKS, R4 DOOR FWD CABLE JUMPED PULLEY AND IS DAMAGED. DEPRESSURIZED DOOR ASSIST BOTTLE. REMOVED PULLEY FOR R4 DOOR LOWER CABLE DRIVE UNIT, R4 DOOR LOWERING CABLE HAS 4 STRANDS BROKEN IN A 1" AREA. IAW AMM 20-20-06-2 THE NYLON COATING IS NOT BUNCHING UP OR SNAGGING ON ANY PULLEYS. R4 DOOR AND CABLES FUNCTION CHECKS GOOD. R4 DOOR FWD UPPER AND LOWER CABLE REMOVED AND REPLACED IAW MM 52-12-08-2-2, REV 70.0. CABLE TENSION ADJUSTMENT CHECK CARRIED OUT IAW MM 52-12-00-5-2, REV70.0. FOUND SATISFACTORY. R4 DOOR OPS CHECK CARRIED OUT IAW MM52-12-00-2-2, REV 70.0. FOUND SATISFACTORY.
2010
Part: SENSOR — MALFUNCTIONED (NR 2 SLAT) · airframe 65,972 hrs · 13,673 cycles
LEVEL 2 SLAT DISAG ALERT ON APPROACH. CHECKED LT NR 2, LT NR 4 & RT NR 4 SLAT POSITION SENSOR GAP REF MM 27-84-02-4 & 27-84-03-4. ALL CHECKS NORMAL. PERFORMED PSEU TARGET TEST FOR LT NR 2, LT NR 4 & RT NR 4 REF FIM 31-71 WITH SIDELOAD APPLIED TO EACH TRACK, NO DEFECTS NOTED.
2009
Part: LANDING GEAR — MALFUNCTIONED · airframe 63,653 hrs · 13,108 cycles
AFTER DEPARTURE, FOUND RT MAIN GEAR IND UNSAFE ON GEAR INDICATION LIGHTS AND ON SECONDARY/CONFIG PAGE. UNABLE TO CHECK FLOOR WINDOW BUT NO ABNORMAL VIBRATIONS, ALL INDICATIONS GOOD WITH GEAR DOWN. WHILE FLYING W/GEAR HANDLE UP, CONFIG PAGE SHOWED OCCASIONAL FLAP POSITION INDICATIONS ON RT SIDE OF (BLANK)(0) JACKED ACFT AND PERFORMED GEAR SWING. RT MLG INDICATION OPERATES NORMALLY. REF AMM 07-11-00-2. NOTE: FLAP INDICATION CHECKED NORMAL. NO ACTION TAKEN ON FLAP INDICATION.
Part: PSEU — MALFUNCTIONED (MLG) · airframe 62,500 hrs · 12,859 cycles
ON APPROACH WITH GEAR SELECTED DOWN, RECEIVED NO SAFE GREEN LITE IN EITHER PRI OR SEC INDICATORS. EXECUTED M/A. FOUND "LDG GEAR WARN PRI" CB OUT. RESET CB AGAIN WHICH STAYED IN AND ALL PRI AND SEC INDICATORS NOW SAFE. UNEVENTFUL LANDING FOLLOWED. REMOVED AND REPLACED PSEU IN REF TO MM 31-71-01-2. REMOVED AND REPLACED GEAR POSITION LIGHT MODULE ASSY IAW MM 32-61-11-4 AND C/B B1-415.
Part: FITTING — CRACKED (ZONE 300) · airframe 62,036 hrs · 12,756 cycles
CRACK AT 3 O'CLOCK POSITION FOUND ON LOWEST FASTENER HOLE ON NR 4 BANJO FITTING RT SIDE AFT LOCATION COMMON TO THE CARRY THROUGH CAP. COMPLIED WITH EA NR 1-5530-49623, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 107.
Part: SKIN — MISREPAIRED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
EXISTING REPAIR DOUBLER AT BS 1868-1888 LONGERON 9-10L EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR1-5310-127862, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.
Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 62,036 hrs · 12,756 cycles
EXISTING REPAIR FOUND ON RT WING INBD FLAP UPPER SKIN AT STA. XIFH= 216. FOUND NOT IAW SRM. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 38 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 62,036 hrs · 12,756 cycles
EXISTING REPAIR FOUND ON RT WING INBD FLAP UPPER SKIN AT STA. XIFH= 299. FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 39 VOL I. CLASSIFIED AS A MINOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,036 hrs · 12,756 cycles
FUSELAGE, EXISTING REPAIR DOUBLER AT STA 1853 TO STA 1871 LONGERON 45L TO 48L. EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. REPAIR CARRIED OUT AS PER EA NR1-5310-127861, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,036 hrs · 12,756 cycles
EXISTING REPAIR DOUBLERS AT STA 1900 TO STA 1921 L39 TO L42 RT EVALUATED AND FOUND NOT IN ACCORDANCE WITH THE SRM. REPAIR CARRIED OUT AS PER SRM 53-20-00 FIG. 2 VOL.I. REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, RT STA 5-83, X= -8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, LT STA 5-34, X= 77 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. 1 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SKIN — CORRODED (FUSELAGE) · airframe 62,036 hrs · 12,756 cycles
FUSELAGE, LAVATORY SERVICE ACCESS DOOR CUT-OUT LT AFT SIDE FOUND CORRODED. COMPLIED WITH EA 1-5310-127860, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.
Part: CAP — CRACKED (LT PYLON) · airframe 62,036 hrs · 12,756 cycles
HFEC INSPECTION CARRIED OUT, CRACK APPROXIMATELY 1.5 INCHES LONG FOUND ON THE LT SIDE PYLON UPPER CAP ON RADIUS BETWEEN YID=408 TO YID=410. COMPLIED WITH EA 1-5410-127853, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, LT STA 1491 X= 8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. 1 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, LT STA 5-02, X= 47 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, LT STA 5-72, X= 47 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. 1 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,036 hrs · 12,756 cycles
CABIN, RT STA 5-15 X= -107 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00 FIG 6 VOL. 1 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,036 hrs · 12,756 cycles
CABIN, LT STA 5-53 TO STA 5-93, X= 8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.
Part: BRACKET — DAMAGED (ZONE 500) · airframe 62,036 hrs · 12,756 cycles
LT WING OUTBD FLAP OTBD FWD HINGE PIVOT BORE FOUND WITH SCORING MARK. COMPLIED WITH E.A. 1-5750-129218, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 62,036 hrs · 12,756 cycles
RT WING OTBD FLAP OUTBD FWD HINGE LOWER MOUNT BOTH BORE AFT FACE FOUND WITH CORROSION. COMPLIED WITH EA NR 1-5750-129219, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.
Part: TEE FITTING — CORRODED (LT TE FLAP VANE) · airframe 62,036 hrs · 12,756 cycles
LT WING OTBD FLAP VANE T-FITTING NR 3 FROM INBD ATTACH BORE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-127865, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: TEE FITTING — CORRODED (RT TE FLAP VANE) · airframe 62,036 hrs · 12,756 cycles
RT WING OTBD FLAP VANE T-FITTING NR 5 FROM INBD ATTACH BORE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-127866, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 62,036 hrs · 12,756 cycles
LT WING OTBD FLAP OUTBD FWD HINGE ACTUATOR INBD BORE FOUND CORODED. COMPLIED WITH E.A. 1-5750-129218, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: TEE FITTING — CORRODED (RT TE FLAP VANE) · airframe 62,036 hrs · 12,756 cycles
RT WING OTBD FLAP VANE T-FITTING NR 4 FROM INBD ATTACH BORE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-127867, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 62,036 hrs · 12,756 cycles
RT WING OUTBD FLAP INBD FWD HINGE ACTUATOR INBD BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-129214, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.
Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 62,036 hrs · 12,756 cycles
LT WING INBD FLAP VANE TRAILING EDGE SURFACE FOUND DELAMINATION. LT WING INBD FLAP VANE REMOVED & REPLACED AS PER AMM 27-50-22-4 REV. 62. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.
2008
Part: SKIN — DAMAGED (ZONE 100) · airframe 57,428 hrs · 11,720 cycles
DURING TRANSFERRING OF HOLE FOUND EXTRA FASTENER HOLE. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-117263, TITLE "FUSELAGE MAINFRAME LT AIR CONDITIONER DOOR JAMB SKIN REPAIR". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 500) · airframe 57,428 hrs · 11,720 cycles
02 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. COMPLIED WITH FEDEX E.A. 1-5710-117257, CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 57,428 hrs · 11,720 cycles
06 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=685 AND STA XORS=710. COMPLIED WITH EA 1-5710-117258, CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 200) · airframe 57,428 hrs · 11,720 cycles
MAIN DECK CARGO COMPT, FOUND UNDER FLOOR STRUCTURE WITH CORROSION AT STA 1230, LBL 105". REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-117256, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,428 hrs · 11,720 cycles
LT AIRCON COMPT FOUND SUPPORT ON STA Y=575.00 CORROSION. REPAIR CARRIED OUT AS PER SRM 53-00-01 FIGURE 8 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,428 hrs · 11,720 cycles
LEFT SIDE NOSE LANDING GEAR TRUNNION FITTING FOUND CRACK AT LOWER LONGERON FASTENER HOLE. REPAIR CARRIED OUT AS PER SRM 51-33-01 VOLUME II AND FEDEX EA 1-5310-117251, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: DOOR FRAME — CRACKED (BS 547) · airframe 57,428 hrs · 11,720 cycles
NR 2 AIRCON PACK DOOR CUTOUT BS 547, S-33L FOUND FRAME CRACKED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: TRUNNION — CRACKED (NLG) · airframe 57,428 hrs · 11,720 cycles
NOSE LANDING GEAR LEFT TRUNNION FITTING SUSPECT CRACKED. REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGURE 23 VOLUME I AND FEDEX EA 1-5340-117249. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
2006
Part: SPRING — WEAK (RT MLG) · airframe 52,698 hrs · 10,653 cycles
RT MAIN GEAR SHOWED RED ON CONFIG PAGE AND GEAR HAND L/E WHEN RETRACTED. PERFORMED CHECKLIST. WOULD INDICATE DOWN BUT NOT UP DUMPED 3000 LBS FUEL. RT MLG DOOR LATCH SPRING REMOVED AND REPLACED AS PER STD MAINT PRACTICE. ADJUSTMENT CHECK OUT ON RT MLG UP AND LATCHED PROXIMITY SENSOR AS PER AMM 32-61-15-5 FOUND SATISFACTORY. LDG RETRACTION TEST CHECK OUT 10 TIMES AS PER AMM 32-31-00-5 FOUND SATISFACTORY.
Part: SPRING — WEAK (RT MLG) · airframe 52,698 hrs · 10,653 cycles
RT MAIN GEAR SHOWED RED ON CONFIG PAGE & GEAR HANDLE WHEN RETRACTED. PERFORMED CHECKLIST. WOULD INDICATE DOWN BUT NOT UP. ALSO WITH SLATS EXT & FOOT 20 WOULD GET AN INTERMITTENT AUTOSLAT EXTEND & STICKSHAKE. WITH FLAP 15 HAD INTERMITTENT SLAT DISAG & STICKSHAKE. DUMPED 3000 LBS FUEL. RETURNED TO SIN. FOUND RT LATCH SPRING WEAK. REMOVED AND REPLACED SAME. ADJ CHECK RT MLG UP & LATCHED PROX SENSOR PER AMM LDG RETRACT TEST 10 TIMES GOOD. ACARS MSG SHOWED LT SLAT POS SENSORS 4A & 4B ABNORMAL WITH SLATS EXTENDED. REMOVED AND REPLACED BOTH PER AMM. TEST SLAT POS INDICATION, & STICK SHAKER TESTS PER AMM. ALL TESTS PASSED. RETURNED TO SERVICE.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO SEAT TRACK (STA 1000, RT X=75.25) FOUND EDGE UNDER OPENED FLOOR PANEL CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK (STA 989 TO STA 1049, RT X=75.25) AS PER SRM 53-70-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: PANEL — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO UPPER CARGO COMPT UNDER FLOOR AREA AT LT SLANT PANEL (STA 1361) FOUND SURFACE CORRODED. REPAIR CARRIED OUT PER FEDEX EA 1-5710-102123. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO UPPER CARGO COMPT UNDER FLOOR AREA (STA 1289, RT X=95) FOUND SURFACE CORRODED. REPAIR CARRIED OUT PER FEDEX EA 1-5710-102121, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: LONGERON — CORRODED (ZONE 100) · airframe 52,698 hrs · 10,652 cycles
L51R FOUND CORROSION AT STA 1139 TO STA 1159. CORROSION REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: TANK — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO UPPER CTR TANK UNDER FLOOR AREA STA 1225 FOUND SURFACE CORRODED. REPAIR CARRIED OUT AT MM/D CARGO UPPER CTR TANK UNDER FLOOR AREA AS PER FEDEX EA 1-5710-102122. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: ATTACH ANGLE — CRACKED (ZONE 500) · airframe 52,698 hrs · 10,652 cycles
LT WING FIXED L/E RIB DOUBLER ATTACH ANGLE FOUND DAMAGED AT XOS 669. REPAIR CARRIED OUT AS PER FEDEX EA1-5720-97858, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO UPPER CARGO COMPT UNDER FLOOR AREA (STA 1259, RT X=95) FOUND SURFACE CORRODED. REPAIR CARRIED OUT PER FEDEX EA 1-5710-102120, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO SEAT TRACK (STA 755, RT X=8.5) FOUND EDGE GOUGED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO SEAT TRACK (STA 5/0-5/10, LT X=8.5) FOUND EDGE CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK (STA 5/0-5/10, LT X=8.5) AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,698 hrs · 10,652 cycles
M/D CARGO SEAT TRACK (STA 1365, RT X=8.5) FOUND EDGE CORRODED. CORROSION AT EDGE REMOVED AS PER SRM 51-21-01 VOLUME II AND REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SPAR CAP — CORRODED (ZONE 500) · airframe 52,698 hrs · 10,652 cycles
LT WING REAR SPAR UPPER CAP FOUND CORRODED AT XORS 979-992. REPAIR CARRIED OUT PER FEDEX EA 1-5710-102124.
Part: DUCT — CRACKED (ZONE 500) · airframe 52,698 hrs · 10,652 cycles
LT WING TELESCOPING DUCT CUTOUT I/B AND O/B CORNER FOUND CRACKED. REPAIR CARRIED OUT PER FEDEX EA 1-5730-100707. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: DUCT — CRACKED (ZONE 600) · airframe 52,698 hrs · 10,652 cycles
RT WING TELESCOPING DUCT CUTOUT I/B AND O/B CORNER FOUND CRACKED. REPAIR CARRIED OUT PER FEDEX EA 1-5730-100708. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FUEL TANK — CRACKED (ZONE 500) · airframe 52,698 hrs · 10,652 cycles
CRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 9. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (ZONE 600) · airframe 52,698 hrs · 10,652 cycles
RT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS670. REPAIR CARRIED OUT PER FEDEX EA 1-5730-100709. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
2005
Part: WARNING SYSTEM — ACTIVATED (FUEL QTY SYS) · airframe 48,948 hrs · 9,751 cycles
5 MINUTES AFTER TAKE OFF LAT FUEL IMB.C/W QRH HAD YELLOW NR 3 FUEL QTY LAT FUEL IMBALANCE ALERT EXT LATER FUEL QTY FAULT. C/W QRH. TIP TANK LOW ALERT. C/W QRH AND ALERT EXT TIP TANK LOW ALERT AGAIN, BEGAN QRH THEN GOT TIP TNK TRAPPED ALERT WITH 5700 BELOW ON SD. TURNED ON ALL CROSSFEED VALVES ACCORDING TO QRH. LAT FUEL FUEL IMB ALERT WITH 18000 TANK 1, 8000 TANK 3. BALANCED TANKS BEFORE LANDING. LANDING UNEVENTFUL AT KDEN. T/S NR 3 FUEL QTY SYS AND REPLACED BOTH INNER AND OUTER MJP'S. REPLACED MJP'S PER MD-11 MM 28-41-40-4. LEAKED CHECKED MJP'S. ALL PROBES AND COMPUTERS READ NORMAL FUEL QTY TEST NORMAL. NO TIP TANK TRAPPED WARNINGS OCCURED. SYSTEM OPERATES NORMALLY.
Part: FASTENER — WRONG PART (RT WING SPAR) · airframe 48,638 hrs · 9,684 cycles
RT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 2, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENERS. LOCATION IS BY XORS 570.00. INSTALLED HLT623 TYPE FASTENERS IN LIEU OF THOSE CALLED OUT IN EO 1-5750-7-5004. COMPLIED WITH FEDEX EA 1-5750-82944, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE. TENSION STRAP FASTENER HOLES.
Part: SKIN — PUNCTURED (NR 6 SLAT) · airframe 48,638 hrs · 9,684 cycles
LT WING, PUNCTURED LEADING EDGE SLAT NR 6 AFT FACE SKIN. REPAIRED PER SRM 57-10-00 VOLUME I, FIGURE 1.
Part: FASTENER — WRONG PART (LT WING SPAR) · airframe 48,638 hrs · 9,684 cycles
LT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 1, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENER. LOCATION IS BY XORS= 570.00. INSTALLED HLT623 TYPE FASTENERS IN LIEU OF THOSE CALLED OUT IN EO 1-5750-7-5004. COMPLIED WITH FEDEX EA 1-5750-82944, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE. TENSION STRAP FASTENER HOLES.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK, RIGHT SEAT TRACK AT STA Y= 1454, X=-29 FOUND WITH CORROSION. MAIN DECK, RIGHT SEAT TRACK CUT FROM STA Y= 1411, X=-29 AND REMOVED AT SPLICE AREA PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND REPROTECTED PER 51-21-01 VOLUME II. REPAIR TRACK AND SPLICE INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31- 01 VOLUME II.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
RT SEAT TRACK AT STA Y= 1361 - Y= 1381, X= -29, FOUND WITH CORROSION. MAIN DECK, RIGHT SEAT TRACK AT STA Y= 1351 - Y= 1381, X= -29 CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM SRM 51-31-01 VOLUME II. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR SEAT TRACK AND SPLICE INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK, RIGHT HAND SEAT TRACK AT STA Y= 1361 - Y= 1481, -X= 47 FOUND WITH CORROSION. MAIN DECK, RIGHT HAND SEAT TRACK CUT AND REMOVED FROM STA Y= 1351 - Y= 1481 -X= 47 PER SRM 51-31-01 VOLUME II. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-3102 VOLUME II.
Part: FITTING — CORRODED (ZONE 700) · airframe 48,638 hrs · 9,684 cycles
CENTER LANDING GEAR, RIGHT HAND TRUNNION SUPPORT FITTING SHEAR PIN HOLES FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5340-82950.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1179 TO 1239, WL 75 FOUND WITH CORROSION AEA7325-15.
Part: RIB — CRACKED (TAIL CONE) · airframe 48,638 hrs · 9,684 cycles
EMPENNAGE, EXTENDED TAIL CONE AFT INTERIOR RIB FRAME FOUND CRACKED. REMOVED PER SRM 51-35-01 VOLUME II. NEW RIB AND SPLICES FABRICATED PER DWG AKC7605 AND PART MARKED PER GMM 7-0-1001. NEW RIB AND SPLICES INSTALLED PER SRM 51-35-01 VOLUME II.
Part: FITTING — CORRODED (ZONE 700) · airframe 48,638 hrs · 9,684 cycles
CENTER LANDING GEAR, LEFT HAND TRUNNION SUPPORT FITTING SHEAR PIN HOLES FOUND CORRODED. REPAIR CARRIEDOUT AS PER FEDEX EA 1-5340-82950.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,638 hrs · 9,684 cycles
RT SEAT TRACK AT STA 1500 TO 1531, RBL-75 CORRODED. REPAIRED SEAT TRACK AND SPLICE FABRICATED AS PER SRM 51-70-00 FIGURE 1 VOL I AND INSTALLED AS PER SRM 51-31-01 VOL II.
Part: STRAP — CRACKED (ZONE 500) · airframe 48,638 hrs · 9,684 cycles
LEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACKED, FOUND ON THE SPOTFACE OF THE UPPER BOLT HOLE AT 3 O'CLOCK AND LOWER BOLT HOLE AT 6 O' CLOCK POSITIONS (VIEW LOOKING INBOARD) WITH CRACK. LENGTH APPROXIMATELY ONE-FOURTH (1/4) INCH AND ONE-EIGHTH (1/8) INCH RESPECTIVELY. KIT P/N 1575075004-03. REPLACED PER FEDEX EO 1-5750-7-5004 PART 1.
Part: STRAP — CRACKED (ZONE 600) · airframe 48,638 hrs · 9,684 cycles
RT WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP SUPPORT FOUND CRACKED. KIT P/N 1575075004-0. REPLACED PER FEDEX EO 1-5750-7-5004 PART 2.
Part: STRINGER — CRACKED (ZONE 600) · airframe 48,638 hrs · 9,684 cycles
RIGHT HAND WING STRINGER 10 END SUSPECTED CRACKED ARB7510-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090.
Part: TRUNNION — CORRODED (ZONE 700) · airframe 48,638 hrs · 9,684 cycles
CENTER LANDING GEAR, RT TRUNNION SUPPORT FITTING MATING SURFACE FOUND CORRODED AND EXCEED LIMIT AREA OF 10 PERCENT PER SRM 53-40-00 FIGURE 15, SHEET 4. (FOR LOCAL BLEND OPTIONS) AEA7051-502. REPAIR CARRIED OUT IAW FEDEX EA 1-5340-82950.
Part: TRUNNION — CORRODED (ZONE 700) · airframe 48,638 hrs · 9,684 cycles
CENTER LANDING GEAR, LT TRUNNION SUPPORT FITTING MATING SURFACE FOUND CORRODED AND EXCEED LIMIT AREA OF 10 PERCENT PER SRM 53-40-00 FIGURE 15, SHEET 4, (FOR LOCAL BLEND OPTIONS) AEA7051-501. REPAIRED IAW FEDEX EA 1-5340-82950.
Part: STRINGER — CRACKED (ZONE 600) · airframe 48,638 hrs · 9,684 cycles
RIGHT WING STRINGER 11 END SUSPECTED CRACKED ARB7511-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090.
Part: STRINGER — CRACKED (ZONE 600) · airframe 48,638 hrs · 9,684 cycles
RT WING STRINGER 9 END SUSPECTED CRACKED ARB7509-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,638 hrs · 9,684 cycles
MAIN DECK - SEAT TRACK AT RIGHT HAND STA Y= 1371 TO Y= 1500, X= -75 CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL. I.
Part: STRINGER — CRACKED (LT WING) · airframe 48,638 hrs · 9,684 cycles
LEFT WING STRINGER 13 END SUSPECTED CRACKED. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10.
Part: STRINGER — CRACKED (ZONE 500) · airframe 48,638 hrs · 9,684 cycles
LEFT WING STRINGER 11 END SUSPECTED CRACKED ARB7514-1. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090.
Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA Y= 635, X= 47, FOUND CRACKED APPROXIMATELY THREE (3) INCHES LONG. REMOVED SEAT TRACK IAW SRM 51-31-01 VOLUME II. FABRICATED PARTS IAW SRM 53-70-00 VOLUME I, FIGURE 1. PARTS INSTALLED IAW SRM 50-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-00 VOLUME II.
Part: SPAR CAP — CORRODED (ZONE 600) · airframe 48,638 hrs · 9,684 cycles
RIGHT HAND WING UPPER REAR SPAR CAP FOUND CORRODED AT XORS= 980 ARC7413-2. CARRIED OUT AS PER FEDEX EA 1-5710-82938.
Part: SLIDING SLEEVE — CRACKED (ZONE 400) · airframe 48,638 hrs · 9,684 cycles
NR 2 ENGINE RIGHT THRUST REVERSER COWL UPPER SLIDER TRACK END CRACKED. THRUST REVERSER COWL REMOVED AS PER FEDEX WORKCARD 78T3002-R AND REPLACED AS PER FEDEX WORKCARD 78T3902-R.
Part: BLOCK — CORRODED (ZONE 700) · airframe 48,638 hrs · 9,684 cycles
CENTER LANDING GEAR, LEFT HAND AND RIGHT HAND PILLOW BLOCKS, FOUND EMITTED WITH RUST. LEFT HAND AND RIGHT HAND PILLOW BLOCKS REMOVED AND REPLACED PER CMM 32-15-01. CENTER LANDING GEAR ASSEMBLY REINSTALLED PER WIC 32T9004.
Part: CARGO TRACK — CRACKED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 8.5, FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 & INSTALLED PER SRM 51-31-01 VOL II.
Part: CARGO TRACK — WORN (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 47, FOUND WORN AT CROWN AREA. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 & INSTALLED PER SRM 51-31-01 VOL II.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 27, FOUND CRACK APPROXIMATELY THREE (3) INCHES LONG. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 AND INSTALLED PER SRM 51-31-01 VOL II.
Part: CARGO TRACK — CRACKED (ZONE 200) · airframe 48,638 hrs · 9,684 cycles
MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 8.5, FOUND CRACKED APPROXIMATELY THREE (3) INCHES LONG. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOL I, FIG 1. REPAIR PARTS INSTALLED PER SRM 50-70-00 VOL I, FIG 1 AND SRM 51-31-00 VOL II.
2004
Part: ENGINE — LEAKING (NR 3) · airframe 47,858 hrs · 9,505 cycles
ENGINE 3 OIL QTY DECREASED TO 8 GALLONS AT 4 HOURS AFTER TAKEOFF. QUANTITY DECREASED TO 4 GALLONS EVEN WHILE USING REDUCED POWER ON THAT ENGINE. DIVERTED THE FLIGHT TO EGSS AND QUANTITY WAS AS LOW AS 1 GALLON ON APPROACH. TEMPERATURE AND PRESSURE WERE NORMAL. AFTER LANDING THE ENGINE WAS SHUTDOWN AND QUANTITY INCREASED TO 7 GALLONS.
Part: COALESCER BAG — DIRTY (A/C PACK) · airframe 47,681 hrs · 9,464 cycles
DURING CRUISE FLT AT FL300 250KTS, HAD WHITE SMOKE OMITTING FROM TOP OF GLARESHIELD. REF QRH SMOKE FUMES OF ELECT, AIR COND OR UNKNOWN REASONS, DECLARED EMERG WITH VHHH AND EXPEDITED TO A LANDING AT VHHH. SMOKE DISSIPATED BY LANDING CREW VERBAL NOT ELECT BURN, JUST SMELL OILY AND ACFT ALL SYSTEM WORK NORM. INSP AV COMPT & ALL DU'S INST PNL AREA, ALL WIRING NO DISCREPANCY. INSP ALL 3 PACK'S COALESCER BAG FOUND NR 3 HAS SLIGHT OILY SMELL. PERF AIR COND ODOR DIST DUCT CLEANING PER MM 21-53-00-7.RR ALL 3 COALESCER BAG'S PER 21-54-05-2.C/W THE MTSI INSP ALL 3 ENG 8TH STAGE CHECK VALVE & APU LBV DUCTING NO WET SIGN PER 36-11-01-4 & 36- 16-02. PRECAUTIONARY DEF NR 3 PACK PER MEL 21-51-01-A. ACFT OK FOR SERVICE.
2003
Part: BRACKET — CHIPPED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, FOUND O/B HINGE FITTING I/B EDGE WITH CHIPPED MARK. COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: FITTING — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2.
Part: COLLAR — CRACKED (BANJO FITTING) · airframe 43,779 hrs · 8,576 cycles
LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505 ) AFT FACE FLANGE FOUND WITH 02 EA LOCKBOLT COLLARS CRACKED (GAIN ACCESS FROM PNL 364AR). RIGHT LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505 ) AFT FACE FLANGE 02 EA CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL II AND REPLACED AS PER SRM 51-33-01 VOL II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363PL. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CRACKED (FUSELAGE) · airframe 43,779 hrs · 8,576 cycles
RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. ACCESS FROM PNL 364MR. RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL2
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2 & SRM 51-38-01 VOL2.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 364MR. RT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363BL. LT CENTER SECTION OF NR 1 BANJO FITTING AJC7051-505 AFT FACE FLANGE 1 CRACK LOCKBOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 03 EA LOCK BOLT COLLARS CRACKED. RH CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 AFT FACE FLANGE 3 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND INSTALLED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 3 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363AL. LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 3 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2.
Part: FITTING — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 08 EA LOCK BOLT COLLARS CRACKED.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501 AFT FACE FLANGE 05EA CRACK LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE FOUND WITH 7 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE 7 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361CL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACK LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II AND REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LOWER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT LOWER SECTION OF NR 3 BANJO FITTING AJC7053-503 FWD FACE FLANGE 5 CRACKED LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION BETWEEN NR 1 & 2 BANJO FITTINGS SUPPORT CLIP FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION BETWEEN NR 1 & 2 BANJO FITTING SUPPORT CLIP 2 CRACKED LOCKBOLT COLLARS REMOVED & REPLACED AS PER SRM 51-32-01 VOL2 & SRM 51-33-01 VOL2 RESPECTIVELY.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 04 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 4 CRACKED LOCKBOLT COLLARS REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 3 BANJO FITTING (AJC7053-503) FWD FACE FLANGE FOUND WITH 02 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 3 BANJO FITTING AJC7053-503 FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2 & SRM 51-38-01 VOL2.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
BETWEEN UPPER SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEB FOUND WITH 02EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPP SECTION OF BANJO FITTINGS NR 1 & 2 ATTACHED HORIZONTAL WEBS 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL2 & REPLACED AS PER SRM 51-33-01 VOL2.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLAR CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING (AJC7051-505) FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY.
Part: FITTING — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LEFT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 02EA LOCK BOLT COLLARS CRACKED.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 3 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL 2
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361DL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACK LOCK BOLT COLLAR REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LOWER SECTION OF NR 2 BANJO FITTING (AJC7052- 501) AFT FACE FLANGE FOUND WITH 07 EA LOCK BOLT COLLARS CRACKED. RT LOWER SECTION OF NR 2 BANJO FITTING AJC7052-501 AFT FACE FLANGE 07EA CRACK LOCK BOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II. AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (FUSELAGE) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) AFT FACE FLANGE FOUND WITH 05 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING AJC7052-501AFT FACE FLANGE 5 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II AND SRM 51-38-01 VOL. II.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 2 BANJO FITTING (AJC7052-501) FWD FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB FOUND WITH 03 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 ATTACHED HORIZONTAL WEB 3 CRACKED LOCKBOLT COLLARS REMOVED AND REPLACED AS PER SRM 51-32-01 VOL. II AND SRM 51-33-01 VOL. II.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS (AJC7581-11 & AJC7581-19) FOUND WITH 02 EA LOCKBOLT COLLARS CRACKED. LT BETWEEN UPPER SECTION OF BANJO FITTINGS NR 2 & 3 INTERCOSTAL STIFFENERS AJC7581-11 & AJC7581-19, 02 EA. CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01 VOL. II AND REPLACED AS PER SRM 51-33-01 VOL. II.
Part: COLLAR — CRACKED (STABILIZER) · airframe 43,779 hrs · 8,576 cycles
LEFT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 02 EA LOCK BOLT COLLARS CRACKED. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL.II & INSTALLED AS PER SRM 51-33-01, VOL.II.
Part: COLLAR — MISSING (FUSELAGE) · airframe 43,779 hrs · 8,576 cycles
LOWER SECTION OF NR 1 BANJO FITTING (AJC7051-505) AFT FACE LONGITUDINAL ATTACHED STIFFENER FOUND WITH 01 EA FASTENER MISSING. GAIN ACCESS FROM PNL 364AR. RT LOWER SECTION OF NR 1 BANJO FITTING AJC7051-505 AFT FACE LONGITUDINAL STIFFENER MISSING HEAD FASTENER REPLACED AS PER SRM 51-33-01 VOL2.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 3 LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 3 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CORRODED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 3363RL. LT CENTER SECTION OF NR 4 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 1 LOCK BOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 361EL. LT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE FOUND WITH 9 LOCKBOLT COLLARS CRACKED. GAIN ACCESS FROM PANEL 363CL. LT CENTER SECTION OF NR 1 BANJO FITTING AFT FACE FLANGE 9 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM 51-32-01, VOL. II & REPLACED AS PER SRM 51-33-01, VOL II.
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE FOUND WITH 2 LOCKBOLT COLLARS CRACKED. LT CENTER SECTION OF NR 2 BANJO FITTING FWD FACE FLANGE 2 CRACKED LOCKBOLT COLLARS REMOVED AS PER SRM51-32-01 VOL2 AND REPLACED AS PER SRM51-33-01VOL2
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE FOUND WITH 1 LOCKBOLT COLLAR CRACKED. GAIN ACCESS FROM PANEL 363PL. LT CENTER SECTION OF NR 3 BANJO FITTING AFT FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED AS PER SRM51-32-01 VOL 2 AND REPLACED AS PER SRM51-33-01 VOL 2
Part: COLLAR — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE FOUND WITH 01 EA LOCK BOLT COLLARS CRACKED. RT CENTER SECTION OF NR 1 BANJO FITTING FWD FACE FLANGE 1 CRACKED LOCKBOLT COLLAR REMOVED & REPLACED AS PER SRM 51-32-01, VOL. II & SRM 51- 33-01, VOL II RESPECTIVELY.
Part: FITTING — CRACKED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
RIGHT CENTER SECTION OF NR 1 BANJO FITTING (AJC7051-505) LOWER CORNER OF FWD FACE ATTACHED ANGLE FOUND WITH A HAIRLINE CRACK MEASURED APPROX 0.5 INCH. NDT - HFEC CARRIED OUT ON ANGLE AT RT CENTRE SECTION OF NR 1 BANJO FITTING LOWER CORNER FWD FACE AND FOUND ANGLE CRACK FREE.
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B BUSHING LOOSE & HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
N0318 LT OB FLAP, OB HINGE ACTUATOR HOLE NR 1 I/B CORRODED.COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 4 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE PIVOT HOLE NR 3 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 1 I/B UNFLANGE SIDE CORRODED COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.
Part: FITTING — WORN (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 I/B WITH WORN CHROME PLATING AT HOLE. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 O/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP -OUTBOARD HINGE BRACKET BORE CORRODED.
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 2 O/B WITH WORN CHROME PLATING AT HOLE. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 O/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.
Part: FITTING — CORRODED (LT TE FLAP) · airframe 43,779 hrs · 8,576 cycles
N0304 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
N0310 LT OB FLAP, FOUND OB HINGE PIVOT HOLE NR 3 IB UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 2 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND I/B HINGE PIVOT HOLE NR 3 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT O/B FLAP, O/B HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: FITTING — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 1 FLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED
Part: COLLAR — CRACKED (FASTENER) · airframe 43,779 hrs · 8,576 cycles
AFT FUSELAGE COMPT: AFT BODY BULKHEAD FRONT FACE STA Y2014 CAN NOT BE FOUND WITH MANY LOCK BOLT COLLARS CRACKED AXIALLY AS MARKED. AFT FUSELAGE COMPT : AFT BODY BULKHEAD FRONT FACE STA Y2014 CRACK FASTENERS REMOVED & REPLACED AS PER SRM 51-33--01 VOL2.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RH UPPER AFT PLANK 35R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1- 5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR 1- 5510-7-5000.
Part: KEELBEAM — CANNING (FUSELAGE) · airframe 43,779 hrs · 8,576 cycles
WITH RESPECT TO OIL CANNING INSP AS PER EA 1-5310-55649 REV NO A POS P2 ON RIGHT KEEL WEB STA Y 1431 THRU 1441 BET STA Z -97.00 THRU -78.00 FOUND VALUE MEASURED TO BE 0.320 INCHES (EXCEEDED PER THE STATED 0.190 INCH LIMITS). RE-INSPECTION ON RH KEEL WEB STA Y1431 THRU 1441 BET STA Z -97.00 THRU -78.00 OIL CANNING AS PER EA 1-5310-55649B MEASURED TO BE 0.185 INCH FOUND WITHIN LIMIT.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RH UPPER AFT PLANK 27R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1- 5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000.
Part: BOLT — GOUGED (FAILSAFE) · airframe 43,779 hrs · 8,576 cycles
UPON REMOVAL OF BOLT 36 LT FAILSAFE FOUND BOLT HOLE INNER SURFACE WITH 03 EA GOUGES. COMPLIED WITH FEDEX EA 1-5510-74261 STABILIZERS - HORIZONTAL STABILIZER 36L FAIL-SAFE BORE GAUGED
Part: SKIN — CRACKED (RT WING) · airframe 43,779 hrs · 8,576 cycles
RIGHT WING NR 1 SLAT TRACK CUT OUT I/B SKIN FOUND CRACKED DURING I/B SLAT RIGGING CHECK. RT WING NR 1 SLAT TRACK CUT OUT I/B SKIN CRACK REPAIRED AS PER SRM 57-10-00 FIG 15 VOL1.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER FWD SPAR NR 1R BARREL NUT BORE FOUND CORROSION EXCEEDED EO LIMITATION. HOR STAB RT UPPER FWD SPAR 1R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR 1- 5510-7-5000.
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 1 I/B CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 2 O/B CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 2 O/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT HINGE HOLE NR 4 O/B SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.
Part: STRUCTURE — CORRODED (NR 5 SLAT) · airframe 43,779 hrs · 8,576 cycles
RT OUTBOARD FLAP FOUND VANE TO TRACK ATTACHMENT NR 5 WITH SLOT CORRODED AS MARKED. RT OUTBOARD FLAP VANE TO TRACK ATTACHMENT NR 5 CORROSION REPAIRED AS PER FEDEX EA 1-5750-74257, WING RT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.
Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER FWD SPAR NR 1R BARREL NUT BORE FOUND CORROSION EXCEEDED EO 1-5510-7-5000 LIMITATIONS. HOR STAB RH UPPER FWD SPAR #1R BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000.
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT BOLT HOLE NR 3 I/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBD FLAP FOUND INBOARD HINGE ACTUATOR HOLE NR 1 I/B FLANGE SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER AFT PLANK 35R BARREL NUT BORE FOUND CORROSION EXCEEDED EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STAB RT UPPER AFT PLANK 35 RT BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000.
Part: HINGE FITTING — CORRODED (TE FLAPS) · airframe 43,779 hrs · 8,576 cycles
LEFT INBOARD FLAP FOUND OUTBOARD HINGE FITTING PIVOT HOLE FLANGE LOCATION WITH SURFACE CORROSION AS MARKED. LT I/B FLAP O/B HINGE FITTING PIVOT HOLE FLANGE LOCATION SURFACE CORROSION REPAIRED AS PER FEDEX EA 1-5740-74253, WING - LT & RT I/B TRAILING EDGE FLAP- O/B HINGE BRACKET ASSY CORROSION.
Part: PANEL — CORRODED (LT WING) · airframe 43,779 hrs · 8,576 cycles
LEFT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT FOUND CORROSION. LT WING UPPER SURFACE O/B OF FUEL TANK PANEL 533 AT CORROSION REPAIRED AS PER FEDEX EA 1-5710-74260.
Part: STRUCTURE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RT OUTBOARD FLAP FOUND VANE TO TRACK ATTACHMENT NR 4 WITH SLOT CORRODED AS MARKED. RT OUTBD FLAP VANE TO TRACK ATTACHMENT NR 4 CORROSION REPAIRED AS PER FEDEX EA 1-5750-74256, WING RT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION.
Part: HINGE — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
LT OUTBOARD FLAP FOUND INBOARD HINGE PIVOT BOLT HOLE NR 3 INBOARD SIDE CORRODED AS MARKED. COMPLIED WITH FEDEX EA 1-5750-74254 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER BOLT HOLE I/B FLANGE SIDE CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING LOWER BOLT HOLE I/B FLANGED SIDE CORROSION. R & R AS PER FEDEX EA 1-5740-74250. WINGS - LEFT & RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, OUTBOARD HINGE FITTING ACTUATOR MOUNT HOLE INBOARD CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE O/B CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB LEFT UPPER CENTER PLANK NR 26L BARREL NUT BORE FITTING FOUND CORROSION ON BEARING SIDEWALL SURFACES BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26L FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. DAMAGED 26L FITTING ON HOR STAB LT UPPER CENTRE PLANK 26L REMOVED & REPLACED AS PER SRM 51-33--01 VOL2.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING BARREL NUT BOLT HOLE UPPER CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING BARREL NUT BOLT HOLE LOWER CORRODED AS MARKED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR HOLE MOUNT I/B CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING I/B ACTUATOR HOLE MOUNT CORROSION R & R AS PER FEDEX EA 1-5740-74250. WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: FITTING — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNTING MATING SURFACE CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, I/B HINGE FITTING LOWER MOUNTING MATING SURFACE CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250. WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP, FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE INBOARD CORRODED AS MARKED (WING SIDE). RT WING O/B FLAP, O/B HINGE FITTING ACTUATOR HOLE I/B CORROSION REMOVED AND REPLACED AS PER FEDEX EA 1-5740-74252 TITLE : WINGS - LT & RT O/B FLAP - O/B HINGE BRACKET ASSY CORROSION.
Part: HINGE — CORRODED (TE FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE O/B CORRODED (WING SIDE) N0682 RHW O/B FLAP, I/B HINGE FITTING O/B ACTUATOR MOUNT HOLE CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250 TITLE : WINGS - LEFT & RIGHT O/B FLAP - I/B HINGE BRACKET ASSEMBLY CORROSION.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB LT UPPER CENTER PLANK NR 25L BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STAB LT UPPER CENTRE PLANK 25L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000.
Part: FITTING — CORRODED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STABILIZER RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26R FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000. DAMAGED 26R FITTING ON HOR STAB RH UPPER CENTRE PLANK 26R REMOVED & REPLACED AS PER SRM 51-33--01 VOL2.
Part: SKIN — CORRODED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER FWD PLANK NR 6R BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STABILIZER LT UPPER FWD PLANK NR 5L BARREL NUT BORE FOUND CORROSION ON BOTTOM SURFACE BEYOND EO 1-5510-7-5000 LIMITS. HORIZONTAL STAB LT UPPER FWD PLANK NR 5L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245. HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - 1-5510-7-5000.
Part: SPAR CAP — CORRODED (ZONE 300) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STABILIZER RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACES BEYOND EO 1- 5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 43,779 hrs · 8,576 cycles
HORIZONTAL STAB RIGHT UPPER FWD PLANK NR 2R BARREL NUT BORE FOUND CORROSION ON BOTTOM & SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT INBOARD FLAP FOUND OUTBOARD HINGE UPPER O/B MOUNTING HOLE WING SIDE WITH CORROSION. RT I/B FLAP O/B HINGE UPP O/B MOUNTING HOLE WING SIDE CORROSION REPAIRED AS PER FEDEX EA 1-5740-74253,
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORRODED (WING SIDE). LT OUTBOARD FLAP, INBOARD HINGE FITTING ACTUATOR MOUNT HOLE OUTBOARD CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5740-74250
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE INBOARD FLANGE FACE CORRODED (WING SIDE). LT O/B FLAP INBD HINGE FITTING LOWER MOUNT BOLT HOLE I/B FLANGE FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 NAD DWG ARC0502.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE OUTBOARD FLANGE SIDE CORRODED (WING SIDE). LT O/B FLAP, INBD HINGE FITTING LOWER BOLT HOLE O/B FLANGE SIDE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE MATING SURFACE CORRODED (WING SIDE). LT OUTBOARD FLAP, INBOARD HINGE FITTING LOWER MOUNT BOLT HOLE MATING SURFACE CORROSION REMOVED & REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502.
Part: HINGE — CORRODED (RT WING) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP FOUND OUTBOARD HINGE FITTING ACTUATOR HOLE I/B CORRODED. COMPLIED WITH FEDEX EA 1-5740-74252 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION
Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 43,779 hrs · 8,576 cycles
RIGHT OUTBOARD FLAP FOUND INBOARD HINGE FITTING LOWER MOUNTING MATING SURFACE CORRODED. RT WING O/B FLAP, INBD HINGE FITTING LOWER MOUNTING MATING SURFACE CORROSION REMOVED & REPAIRED AS PER EA 1-5740-74250 TITLE : WINGS - LT & RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT OUTBOARD FLAP, FOUND INBOARD HINGE FITTING ACTUATOR MOUNT HOLE INBOARD CORRODED (WING SIDE). COMPLIED WITH FEDEX EA 1-5740-74250 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
Part: RIB — CRACKED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT WING, FOUND OUTBOARD FLAP STOP FITTING FWD RIB WITH CRACK APPROX 0.125 INCHES IN LENGTH. RT WING O/B FLAP STOP FITTING FWD RIB CRACK REPAIRED AS PER FEDEX EA 1-5750-74244 WING - TRAILING EDGE FLAPS - LT & RT O/B FLAP SECONDARY STOP BOSS REPAIR.
Part: RIB — CRACKED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT WING, FOUND OUTBOARD FLAP, STOP FITTING FWD RIB WITH CRACK. APPROX 0.125 IN LENGTH. LT WING O/B FLAP STOP FITTING FWD RIB CRACK REPAIRED AS PER FEDEX EA 1-5750-74244 WING - TRAILING EDGE FLAPS - LT & RT O/B FLAP SECONDARY STOP BOSS REPAIR.
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT INBOARD FLAP, FOUND OUTBOARD HINGE PIVOT HOLE NR 1 OUTBOARD FLANGED SIDE CORRODED. RT I/B FLAP O/B HINGE PIVOT HOLE NR 1 O/B FLANGED SIDE CORROSION REPAIRED AS PER FEDEX EA 1-5750-74251, WING - RT I/B TRAILING EDGE FLAP- HINGE BRACKET CORRODED.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 OUTBOARD CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 O/B CORROSION REMOVED & REPLACED AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 INBOARD FLANGE SIDE CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 I/B FLANGED SIDE CORROSION. R & R AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT INBOARD FLAP, OUTBOARD HINGE, FOUND PIVOT HOLE NR 1 INBOARD CORRODED. RT I/B FLAP O/B HINGE PIVOT HOLE NR 1 I/B CORROSION REPAIRED AS PER FEDEX EA 1-5750- 74251, WING - RT I/B TRAILING EDGE FLAP- HINGE BRACKET CORRODED.
Part: HINGE — CORRODED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE NR 1 INBOARD CORRODED. LT WING I/B FLAP, O/B HINGE PIVOT HOLE NR 1 I/B CORROSION R & R AS PER FEDEX EA 1-5750-74248. WINGS - LEFT I/B TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
Part: HINGE — CORRODED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RIGHT INBOARD FLAP, OUTBOARD HINGE, FOUND PIVOT HOLE NR 1 OUTBOARD CORRODED. RT INBOARD FLAP, OUTBOARD HINGE, PIVOT HOLE NR 1 OUTBOARD CORROSION REPAIRED AS PER EA 1-5750-74251.
Part: RIB — CRACKED (ZONE 500) · airframe 43,779 hrs · 8,576 cycles
LEFT WING LEADING EDGE NR 16 SLAT TRACK INBOARD RIB WITH CRACK. LT WING LEADING EDGE NR 16 SLAT TRACK INBOARD RIB CRACK REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM513301VOL 2.
Part: RIB — CRACKED (ZONE 600) · airframe 43,779 hrs · 8,576 cycles
RT WING LEADING EDGE NR 16 SLAT TRACK INBOARD WEB SUSPECT CRACK. RT WING L/E EDGE NR 16 SLAT TRACK I/B CRACKED RIB REMOVED & REPLACED AS PER SRM 51- 33-01 VOL 2.
Part: VANE — FAILED (TE FLAP) · airframe 40,832 hrs · 7,891 cycles
NR 2 HYDRAULIC SYSTEM FAILED ON TAXI IN. DURING POST FLIGHT INSPECTION, FOUND LEFT, INBOARD FORE FLAP SPLIT IN HALF AT MID TRACK POSITION (LEFT HALF SEPARATED FROM AIRCRAFT). THIS CAUSED FLAP TO CONTINUE BEYOND ITS STOP DURING RETRACTION AND CONTINUED INTO WING INNER TRAILING EDGE STRUCTURE AND HYDRAULIC LINES. LT INBD FLAP VANE INBD TRACK ASSY REPLACED LT INBD FLAP VANE CENTER TRACK & SPRING CARTRIDGE ASSY. REPLACED LT INBD FLAP VANE OTBD TRACK ASSY REPLACED LT INBD FLAP VANE ASSY R & R DAMAGED STRUTS MPN ARC0457507 & 507 ON WING TE STRUCTURE PER MD11 SRM/SMP. AIRCRAFT OK FOR SERVICE. LT INBD FLAP VANE ASSY ADJUSTMENT AND TEST CARRIED.
2002
Part: BOLT — CORRODED (T/E FLAP) · airframe 39,199 hrs · 7,518 cycles
RIGHT WING I/B TRAILING EDGE FLAP LOWER O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289.
Part: BOLT — CORRODED (T/E FLAP) · airframe 39,199 hrs · 7,518 cycles
LEFT WING I/B TRAILING EDGE FLAP LWR O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289.
Part: BOLT — CORRODED (T/E FLAP) · airframe 39,199 hrs · 7,518 cycles
LEFT WING INBOARD T/E FLAP LWR I/B HINGE BOLT CORRODED.
Part: BOLT — CORRODED (T/E FLAP) · airframe 39,199 hrs · 7,518 cycles
RIGHT WING I/B TRAILING EDGE FLAP LWR I/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM 57-51-01-4.
2001
Part: FAIRLEAD — BROKEN (FLIGHT CONTROL) · airframe 35,472 hrs · 6,669 cycles
MAIN DECK CONTROL CABLE FAIRLEAD FOUND BROKEN AT BS 575, RBL 30 BELOW FLOOR PANEL.
2000
Part: FITTING — CRACKED (FUSELAGE) · airframe 31,250 hrs · 5,732 cycles
SNRM 531, EDDY CURRENT INSP NR 4 BANJO FITTING CRACKED. SNRM 570 BANJO 4 FITTING LT AFT MID HOLE EXCEED MAX. REWORK HOLE . ** S/D ** R&R PER 55-20-00 FIG 3 VOL 1 & SB MD-11-55-013 & FEDEX EO 1-55-10-7-3304 & EA 4-5530-49623
Part: BRAKE — FAILED (MLG)
BRAKE ASSY WAS RECEIVED FROM AIR CARRIER ON 2-21-00 FOR REPAIR AND OVERHAUL SERVICE. UPON DIS-ASSEMBLY, IT WAS IDENTIFIED THE AFFECTED BRAKE SUFFERED AN EXTREME CARBON OXIDATION BREAKDOWN ON THE INNER DIAMETER OF THE HEAT SINK. SUBMITTER RECOMMENDATION WOULD BE AN ANALYSIS OR REVIEW OF CARBON COMPOSITE MANUFACTURING PROCESSES. (X)
Part: HARNESS — MALFUNCTIONED (NR 1 ENGINE)
DURING ROLLOUT FIRE ALERT NR 1 ENG. ACCOMPLISHED ENG FIRE CKLIST, USED AGENT 1. AGENT 2 WOULD NOT FIRE. REMOVED AND REPLACED LT AND RT FIRE DET HARNESSES REF MM 71-50-04-4. NR 1 ENG FIRE WARN TEST OK PER MM 26-11-02-5. SEE MTSI 26-11-3714 FOR ADD'L INFO.
Part: FIRE BOTTLE — FAILED (NR 1 ENGINE)
NR 2 FIRE BOTTLE FAILED TO DISCHARGE DURING NR 1 ENG FIRE WARN. RESECURED PIN PER MM 20-30-05-2, ENG 1 AGENT 2 LOW LIGHT FUNCTIONAL CHECK NORM PER MM 26-21-00-0 PARA 7.
1999
Part: ACM — INOP (NR 2)
ON CLIMBOUT, RECEIVED SEL AIR SYS MAN. CREW NOTICED NR 1 PACK TEMP INCREASING AND 3 MIN LATER AIR MANF 1 FAIL LEVEL 3 ALERT. ENG 1 BLD SHOWED CLOSED AND 1-2 ISOL & 1-3 ISOL SHOW CLOSED. *S/D* REMOVED AND REPLACED NR 2 ACM PER MM 21-53-21-2. OPS CK OK MEL IS CLEARED.
Part: ENGINE — MALFUNCTIONED (NR 3)
99-89 - NR 3 ENG N1 INTERMITTENTLY DROPS AND A/C SHUDDERS. REMOVED AND REPLACED NR 3 ENG AS PER MM 71-00-02-4. REF WORK CARD 71T0101.
1998
Part: PRECOOLER — FAILED (PNEU SYSTEM)
DURING CLIMB, AIR MANIFOLD NR 2 FAIL ALERT CAME ON, W/I 10 TO 15 SECONDS OF THE NR 2 MANIFOLD FAIL ALERT, GOT THE NR 3 BLEED AIR OFF ALERT. FOUND THE PRECOOLER LEAKING INTERNALLY. REMOVED AND REPLACED THE PRECOOLER, ALSO REMOVED AND REPLACED 14A AND B MANIFOLD SENSE ELEMENTS, MANIFOLD DECAY CHECK WAS GOOD PER THE JRH.
Part: PIN — INSTALLED (CTR MLG)
CENTER GEAR W/N RETRACT AFTER T/O. RED TABS C/W RETURNED TO MEM. REMOVED L/GEAR PIN FROM CENTER GEAR.
1997
Part: RADIO ALTIMETER — FAILED (LT COCKPIT)
97-0252 - ON CLIMB-OUT LOST ATS THEN BOTH AUTOPILOTS ON DESCENT GOT CONTINUOUS GPWS PULL TERRAIN. ON APPROACH LOC CAPTURE THEN LOST TO HEADING-GS WOULD NEVER CAPTURE LOST FD LOC COMMAND BAR. ON CFDS INTERROGATION, SYS FAULTED RA1 AND RA2 IN FDD 1 FCC 1 AND GPWC RTS TEST PASSED. IN FCC2, FCC2 AND GPWC RTS TESTS PASSED. PER MOCC/MDC REQUEST: REMOVED AND REPLACED NR 1RA PER MM 34-42-01-OPS CK NORMAL. TESTED RA2-SYS OPS NORMAL. C/W RA RECV/TRAN LEAK TEST PER MM 34-42-01 SYS OPS NORMAL, RECONFIGURED A/C PERF AFS AUTOLAND TEST ON FCC1 AND FCC2 SYS OPS NORMAL, TESTS PASSED. A/C STATUS REMAINS CAT 3A.