N306FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
167 reports on file, 1998-03-31 – 2022-11-29.
Part: ENGINE — FIRE (NR 1) · airframe 78,140 hrs · 27,412 cycles
DURING ENGINE 1 START SEQUENCE, ENGINE TOOK LONGER THAN NORMAL TO START. IGNITER USED WAS B, SWITCHED TO A DURING START. ENGINE APPEARED TO START NORMALLY, BUT GROUND CREW ANNOUNCED OVER HEADSET THAT THE AIRPLANE WAS ON FIRE AND TO EVACUATE THE AIRPLANE. WE COULD NOT COMMUNICATE FURTHER WITH GROUND CREW, SO ENGINE SHUTDOWN WAS ACCOMPLISHED INITIALLY WITH FUEL LEVER AND SUBSEQUENTLY FIRE HANDLE. ENGINE 1 FIRE BOTTLE WAS BLOWN DURING EVAC PROCESS. R & R NR 1 ENGINE ALL WORK ACCOMPLISHED IAW ENGINE CHANGE TASK CARD 71T0101-1. ENGINE RUNS COMPLETED. ALL CHECKS NORMAL.
Part: BULB — NO TEST (L1 SLIDE SWITCH) · airframe 77,856 hrs · 27,285 cycles
ON ARRIVAL EVACUATE SLIDE REMOTE PRESS TO TEST INDICATION SWITCH L1 DOOR LIGHT INOP. REPLACED BULBS IN L1 DOOR INDICATOR PRESS TO TEST SWITCH IN REF TO AMM 25-61-03-5-0, OPS CHECKS GOOD AT THIS TIME , LIGHTS WORKED FINE, NO PROBLEM NOTED BY MX AT THIS TIME, OK FOR SERVICE.
Part: WARNING MESSAGE — ILLUMINATED · airframe 77,558 hrs · 27,146 cycles
UNEVENTFUL FLIGHT FROM SMF UNTIL ALERT. LEVEL AT FL310 APROX 2 30 INTO FLIGHT. COST INDEX 200 GAVE US .837MACH. GOT TRI-TONE AND MASTER WARNING LIGHT, WITH "LWR AFT CRG FIRE". DECLARED EMERGENCY AND DIVERTED TO CLOSEST FIELD KTUL. 13MIN FROM DECLARATION TO TOUCHDOWN. STOPPED ON RWY18L MID-FIELD. ALL ENGINE AND APU FIRE BOTTLES WERE DISCHARGED. ALSO, BOTH LOWER CARGO FIRE BOTTLES WERE EXPENDED. EGRESS WAS VIA 1L. SLIDE DEPLOYED NORMALLY, AND BOTH CREW AND 1 JUMPSEATER SAFELY EGRESSED THE A/C. REMOVED CARGO FROM LOWER CENTER AND AFT CARGO COMPARTMENTS. FIRE DEPT PERFORMED INSPECTION AND DID NOT FIND ANY EVIDENCE OF SMOKE OR FIRE. NO EVIDENCE OF SMOKE AND FIRE IN ANY OF THE CARGO REMOVED. DURING OFF LOAD FOUND A SWARM OF "LADY BUGS" IN BOTH COMPARTMENTS SUSPECT SMOKE DETECTORS CONTAMINATED BY THE BUGS. ALSO PERFORMED TROUBLESHOOTING IAW MD10-30 FIM 26-14-00-810-802 AND FOUND ALL SMOKE DETECTORS OPERATING NORMAL. AIRCRAFT DISINSECTION PROCESS WAS PERFORMED IN CENTER AND AFT LWR CARGO COMPARTMENTS IAW MM 12-22-01-2-99 PRIOR TO R&R OF SMOKE DETECTORS. NO MORE EVICENCE OF LADY BUGS PRESENT.
Part: NONE — NONE (N/A) · airframe 77,081 hrs · 26,920 cycles
DESCENDING INTO KMEM WITH FSC IN MANUAL, WE RECIEVED LEVEL 1 ALERT, TANK 3 QTY LO. FUEL WAS 7.1/6.2/5.2. THE QRH SAID TO TREAT AS REAL SO WE DECLARED AN EMERGENCY AND LANDED. AT SHUTDOWN FUEL QTYS WERE 5.9/5.3/3.9. RETERMINTATED WIRES 3E901Z22BL, 3E901AA22BL, 3E900AB22BL, 3E900AC22BL, 3E900AD22BL, 3E900AE22BL, 3E900Y22BL, AND 3E901Y22WH I/A/W MD 11 SWPM 20-10-13 AND CONNECTED TO OUTBOARD MJP. MJP STILL REQUIRES INSTALLATION AND CIRCUIT BREAKERS RESET. INSTALLED #3 TANK OUTBOARD MJP & APPLIED SEALANT TO THE #3 INBOARD MJP REF. AMM 28-41-02-2. NO LEAKS NOTED. VERIFIED #3 TANK DRY CAPACITANCE READINGS ARE WITHIN RANGE REF. AMM 28-41-00-6. VERIFIED #3 TANK BY FUELING TO A KNOWN QUANITY FROM THE #2 TANK. ALL READINGS GOOD REF. AMM 28-00-00-2. AIRCRAFT OK FOR SERVICE.
Earlier reports · 1998–2021 · 163 reports
2021
Part: NONE — NONE (N/A) · airframe 76,774 hrs · 26,776 cycles
THIS CARD IS CREATED FOR TRACKING PURPOSES TO CREATE A RDR/SDR FOR THE REPAIR DONE TO MCD LOWER JAMB AT STA. 697.87 UNDER E.A.8-5330-T0365660 B PART 2 CREATED RDR/SRD FOR MCD LOWER JAMB REPAIR USING E.A. 8-5330-T0365660 B PART 2.
Part: RIB — CRACKED (RT WING) · airframe 76,428 hrs · 26,611 cycles
RIGHT HAND WING - LOWER SURFACE - SECONDARY STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). REPAIRED RIB PER EA.8-5710-T0363338
Part: PANEL — CORRODED (LT WING) · airframe 76,428 hrs · 26,611 cycles
L/H WING PANEL 541LB L/E LAND CORROSION AROUND SCREW HOLE.(MARKED) REMOVED CORROSION , .118 REMAINING THICKNESS, .132 ORIGINAL THICKNESS, .012 MATERIAL REMOVED PER SRM 57-00-01 VOL I , WITHIN LIMITS. TREATED AND PAINTED SRM REF 51-21-01 VOL II.
Part: SUPPORT — WORN (NR 6 SLAT TRACK) · airframe 76,428 hrs · 26,611 cycles
RIGHT WING L/E #6 SLAT TRACK SUPPORT STRUCTURE GOUGED BY FWD O/B RUB BLOCK. (DOT 4) ACCOMPLISHED EA 8-5710-T0362811 WINGS - BASIC WING STRUCTURE - RH WING SLAT TRACK #6 SUPPORT OUTBD RIB AT XOS431 - GOUGE.
Part: PANEL — CRACKED (CARGO DOOR) · airframe 76,428 hrs · 26,611 cycles
PANEL ACA3213 (231LF) CRACK ALONG ONE OF THE HOLES. FABRICATED A NEW PANEL.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 76,428 hrs · 26,611 cycles
DELAMINATED FLOOR PANEL, MAIN UPPER CARGO [L/H, O/B ][STA 600-695]. REMOVED AND REPLACED DELAMINATED FLOOR PANEL REF SRM 51-31-01 VOL2
Part: RIB — CRACKED (ZONE 200) · airframe 76,428 hrs · 26,611 cycles
RIB CRACKED REMOVED AND FABRICATED NEW RIB AND INSTALLED PER DOUGLAS DWG ANB7143 AND SRM 51-31-00 VOL 2
Part: SKIN — WORN (RT WING LE) · airframe 76,428 hrs · 26,611 cycles
R/H WING FIX L/E O/B SIDE HAS WORN MARK FROM SLAT # 2 RUBBING AGAINST IT. LOCATION OF DAMAGE IS ON TOP I/B SIDE STA. XORS 160. REPAIRED PER SRM 57-10-00 VOL 1 FIG 15A.
Part: SKIN — CORRODED (BS 1926-1942) · airframe 76,428 hrs · 26,611 cycles
CORROSION AT STA.1926-1942 L47-49 BELOW AFT CARGO DOOR. REPAIRED CORROSION AT STA.1926-1942 L47-49 PER EA #T 8-5310-T0362734 TITLED: FUSELAGE - MAINFRAME - SKIN STA 1910-1942, L48 - L44 AFT CARGO DOOR UNDER SCUFF PLATE - CORRSION
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,428 hrs · 26,611 cycles
LOWER FUSELAGE AFT CARGO PANEL 187FF DELAMINATED P/N AGA3877-15 FABRICATED NEW LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187FF P/N AGA3877- 15 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 76,428 hrs · 26,611 cycles
FLOORBOARD SR84852-125 DAMAGED. FABRICATED FLOORBOARD SR84852-125 PER FEDEX DRW SRZ-25-001
Part: BRACKET — CRACKED (RAM AIR INLET) · airframe 76,428 hrs · 26,611 cycles
#3 ACM RAM AIR INLET SHELL BRACKET THAT IS MOUNTED BELOW THE AVIONINCS RACK IS BROKEN. REMOVED & REPLACED BRACKET REF ABA7221 & MD10-30 SRM 51-33-01 VOL II.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,428 hrs · 26,611 cycles
LOWER FUSELAGE AFT CARGO FLOOR BOARD PANEL 187BF P/N AGA7428-7 IS DELAMINATED AND MISSING INSERTS FABRICATED LOWER FUSELAGE AFT CARGO FLOOR PANEL 187BF P/N AGA7428-7 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,428 hrs · 26,611 cycles
LOWER FUSELAGE AFT CARGO PANEL 187CF DELAMINATED P/N AGA7429-9 FABRICATED LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187CF P/N AGA7429-9 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
Part: FLOORBOARD — DELAMINATED (FWD CARGO) · airframe 76,428 hrs · 26,611 cycles
LWR FWD PIT FLOOR BOARD 123KF DAMAGED FABRICATED PANEL PER FEDEX DRAWING SRZ-25-005
Part: SKIN — DENTED (BS 1790 L34L) · airframe 76,428 hrs · 26,611 cycles
AFT-INTERMEDIATE/CENTER CARGO - AT APX STA 1790 L34 AFT OF CTR CARGO DOOR, DENT IS PRESENT (TOP DENT). 0000098319 : NAVARRO, ENRIQUE S - 08-JUL-2021 18:25 REPAIRED DENT IN REFERENCE TO MD10-30 SRM 53-20-00 FIG 6 SHEET 7 VOL 1. MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 76,428 hrs · 26,611 cycles
CENTER CARGO FLOOR BOARD 183YF IS DAMAGED FABRICATED CENTER CARGO FLOOR PANEL 183YF REF FEDEX DRAWING SRZ-25-005
Part: FLOORBOARD — DELAMINATED · airframe 76,428 hrs · 26,611 cycles
DELAMINATION ADA0238-9 (127BF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 76,428 hrs · 26,611 cycles
DELAMINATION ADA0244-13 (127EF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
Part: FLOORBOARD — DAMAGED · airframe 76,428 hrs · 26,611 cycles
DAMAGED FLOORBOARD ADA8349-3 (242DF) FABRICATED PER FEDEX DRAWING SRZ-25-005.
Part: SKIN — DELAMINATED (RT WING TE) · airframe 76,428 hrs · 26,611 cycles
R/H TRAILING EDGE PANEL 641HB FOUND TO HAVE DELAMINATION AFTER REMOVAL, MARKED AREA IN RED REPAIRED R/H TRAILING EDGE PANEL 641HB AT THE MARKED DELAMINATED AREA REF SRM 51-71-00 VOL 2 PAGE 3 TO PAGE 47 AND DOUGLAS DRAWING ARC0258
Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 76,428 hrs · 26,611 cycles
DAMAGE FLOOR BOARD AGA7078-70(292EF). FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005.
Part: NUT PLATE — DAMAGED (VERTICAL STAB) · airframe 76,428 hrs · 26,611 cycles
NUMEROUS NUT PLATES DAMAGED INSIDE ZONE 316 R/H UPPER SIDE. AFTER FURTHER INSPECTION CORROSION WAS FOUND AND DETERMINED OUT OF LIMITS. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-00 #24 AND EA NO. 8-5330-T0362493. REPLACED NUT-PLATES IAW SRM 51-31-01 VOL. 2.
Part: BRACKET — CRACKED (WG-BDY FAIRING) · airframe 76,428 hrs · 26,611 cycles
LH WING UPPER SURFACE, FUSELAGE STA.1273 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF ANB7138 DAC DWG.
Part: BRACKET — CRACKED (WG-BDY FAIRING) · airframe 76,428 hrs · 26,611 cycles
LH WING UPPER SURFACE, FUSELAGE STA.1321 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG ANB7141 & MD10-30 SRM 51-33-01 VOL II
Part: BRACKET — CRACKED (BS 1341) · airframe 76,428 hrs · 26,611 cycles
LH WING UPPER SURFACE, FUSELAGE STA.1341 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG ANB7142 & MD 10-30 SRM 51-33-01 VOL II
Part: SKIN — WORN (RT WING DROOP) · airframe 76,428 hrs · 26,611 cycles
R/H WING DROOP LEADING EDGE FLEX SKIN ASSY (PN:ARB2404-3) HAS WORN SLOT HOLE ON SKIN (MARKED). 0004002945 : FICKES, KYLE S - 15-JUN-2021 23:15 REMOVED DAMAGED SLOTTED FLEX SKIN AND REPLACED WITH NEW FABRICATED SKIN REF. MD10-30 SRM 57-10-00 VOL.1 PG.191 FIG.58 SHEET 1 REPAIR OPTION A AND DAC. DWG. ARB2404, SRM 51-31-01 VOL.2 (REFER TO ATTACHED JPF FOR MORE DETAILS) "MAJOR REPAIR"
Part: BRACKET — CRACKED (WG-BDY FAIRING) · airframe 76,428 hrs · 26,611 cycles
LH WING UPPER SURFACE, FUSELAGE STA.1298 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF DAC DWG ANG7139.
Part: FLOOR SUPPORT — CORRODED (BS 1856 RBL 85) · airframe 76,428 hrs · 26,611 cycles
AFT CARGO COMPT RH TUNNEL STA 1853 RBL 85 MAIN DECK FLOORBOARD SUPPORT CORRODED. MRKD REMOVED, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AGA3814-34 REF. DRAWING AGA3814 AND SRM 51-33-01 VOL.2.
Part: STRIKER — WORN (AFT PAX DOOR) · airframe 76,428 hrs · 26,611 cycles
AFT FUSELAGE COMPT DOOR, LATCH INNER STRIKER SURFACE WORN AT MARKED POSITIONS. REPAIRED PER REF E.A 8-5330-T-0362904 :FUSELAGE- PLATES & SKINS - ACCESS DOOR 311AB CUTOUT- DAMAGED DOUBLER. REF MD10-30 SRM VOL II 51-31-01 & MD10-30 SRM 10-30 VOL II 51- 33-01.
Part: DOUBLER — CRACKED (RT WING) · airframe 76,428 hrs · 26,611 cycles
RH WING LE INTERNAL STRUCTURE AT APPROX XORS 555 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH NDT HFEC AND ENDS MARKED. INSTALLED REPAIR DOUBLER, REF EA: # 8-5710-T0362282.
Part: FLOORBOARD — DAMAGED (BS 1561-1661) · airframe 76,428 hrs · 26,611 cycles
AFA3200-2 DAMAGED FABRICATED PER DRAWING SRZ-25-005
Part: DOUBLER — CRACKED (RT WING) · airframe 76,428 hrs · 26,611 cycles
RH WING LE INTERNAL STRUCTURE AT XORS 683 - BEADED DOUBLER IS CRACKED AT TWO (2) LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED REPAIR DOUBLER, REF SRM 57-10-00 FIG 71, VOL 1.
Part: SKIN — CRACKED (LT WING) · airframe 76,428 hrs · 26,611 cycles
L/H WING SKIN AT THE SLAT ANTI-ICE DUCT CUT OUT UPPER INBOARD CORNER HAS A .400 IN. CRACK (MARKED) REPAIRED NOTED CRACK AS REQUIRED PER SRM REQUIREMENTS REF SRM 57-10-00 VOL 1 FIG 103 PG 483-488
Part: SKIN — WORN (BS 695) · airframe 76,428 hrs · 26,611 cycles
LH FUSELAGE STA 695 SKIN HAS GOUGE AT MAIN CARGO DOOR CUTOUT. MRKD AT LWR JAMB AFT OF LATCH SPOOL #4 REPAIRED PER EA # 8-5330-T0362732 P1
Part: FORMER — CRACKED (LT WING) · airframe 76,428 hrs · 26,611 cycles
LH WING LE INTERNAL STRUCTURE AT XORS 562 AND APPROX 18" AFT OF LE - FORMER/FRAME IS CRACKED APPROX .750" IN LENGTH. CRACKED CONFIRMED WITH HFEC AND ENDS MARKED. REPLACED DOUBLER REF DAC DWG ARB3954 & SRM 51-33-01 VOL II MD10-30
Part: BEAM — CRACKED (BS 595 BULKHEAD) · airframe 76,428 hrs · 26,611 cycles
FWD LWR CARGO COMPT STA 595 BULKHEAD BEAM NCA 6044 CRACKED 4 PLACES. MRKD X DIM -5 AND 5 TWO PLACES EACH. Z DIM -59.38 CORRECTION Z DIM SHOULD REA -80 REPAIRED BULKHEAD BEAM NCA6044-29 AT NOTED LOCATION REF. SRM 53-40-00 VOL. 1 FIG. 36 SHEETS 1-4 PGS. 143-146
Part: DOUBLER — CRACKED (LT WING) · airframe 76,428 hrs · 26,611 cycles
LH WING LE INTERNAL STRUCTURE AT XORS 562 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED DOUBLER REF MD10-30 SRM 57-10-00 VOL 1 PG 222 FIG 71 MAJOR REPAIR
Part: SEAT TRACK — WORN (BS 1255-1310) · airframe 76,428 hrs · 26,611 cycles
MAIN CARGO DECK, STA. 1265, LBL 27.50", SEAT TRACK APROX 16" SECTION WORN. DOT #79 REPLACED DAMAGED SEAT TRACK FROM STA 1255 TO 1310 LBL 27.5 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
Part: WEB — CRACKED (BS 472) · airframe 76,428 hrs · 26,611 cycles
NOSE W/W, STA 472, RH WEB NCA6046-3 IS CRACKED JUST BELOW THE REPAIR DOUBLER / ABOVE HORIZONTAL STIFFENER(MARKED). THE CORRECT PART NUMBER FOR THE WEB IS NCA6246-3 0005108155 : SHERWIN, SAMUEL M - 14-JUN-2021 07:28 REPAIRED NOSE W/W, STA 472, RH WEB REF SRM 53-40-00 FIG 34 VOL 1, SRM 51-33-01 VOL 2 MAJOR REPAIR 0000224100 : DE LA GARZA, ADRIAN - 14-JUN-2021 07:30 BUY BACK
Part: SEAT TRACK — WORN (BS 1265) · airframe 76,428 hrs · 26,611 cycles
MAIN CARGO DECK, STA. 1265, LBL 8.50", SEAT TRACK WORN. DOT #9 REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
Part: SEAT TRACK — WORN (BS 1255) · airframe 76,428 hrs · 26,611 cycles
MAIN CARGO DECK, STA. 1255, LBL 8.50", SEAT TRACK WORN. DOT #67. REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
2020
Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 75,069 hrs · 25,918 cycles
ON DESCENT NR 2 ENGINE EGT EXCEEDANCE 1007*C, PRECAUTIONARY SHUT DOWN. NO OTHER EXCEEDANCES, EGT GAUGE "X'D" OUT SEVERAL TIMES. WHEN TROUBLESHOOTING EGT HARNESS PER AMM 77-21-01-2, FOUND UPPER HARNESS LEAD HAD NORMAL, THEN HIGH THEN OPEN RESISTANCE WHEN SHAKING WIRES. CHECK NEW LEAD HARNESS AND WAS STEADY AT CORRECT RESISTANCE 7.2 OHMS. INSTALLED NEW HARNESS AND RAN NR 2 ENGINE AND HAD STEADY EGT READINGS AT NORMAL LEVELS PER JRH. LEAD EGT MANUFACTURE PART 8TK34ACA2, CPN 7700009 AND SERIAL DTA6166.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,879 hrs · 25,827 cycles
ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IN REF TO MD10 SRM 53-20-00 CLASS 2 REPAIR FIG 6. INSTALLED REPAIR PARTS IAW MD10 SRM 53-20-00 FIGURE 6, CLASS 2 REPAIR.
Part: SKIN — DENTED (NOSE AREA) · airframe 74,879 hrs · 25,827 cycles
ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IAW SRM 53-20-00 CLASS 2 REPAIR FIG 6. INSTALLED REPAIR PARTS IAW SRM 53-20-00 FIGURE 6, CLASS 2 REPAIR.
2019
Part: SWITCH — FAULTY (LANDING GEAR) · airframe 73,932 hrs · 25,333 cycles
UPON GEAR RETRACTION ALL THE PRIMARY GEAR AND SECONDARY LIGHTS ILLUMINATED WITH THE GEAR HANDLE UP. FOLLOWED QRH PROCEDURES AND THE GEAR RETRACTED. TROUBLESHOOT IAW FIM 32-30-00-2, PIN A AND B, DID NOT READ CONTINUITY ON SW S1-392. REMOVED AND REPLACED LANDING GEAR FREE FALL SW IAW MM 32-61-04. WITH GEAR PINS INSTALLED, PLACED GEAR HANDLE IN UP POSITION, ALL INDICATIONS ARE NORMAL. SWITCH SW S1-392 P/N H20-24B.
Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 73,749 hrs · 25,227 cycles
AFT FUSELAGE DOOR 311AB CUTOUT SEAL DAMAGED AT AFT SIDE OF OPENING. REPAIRED AFT FUSELAGE DOOR 311AB CUTOUT LATCH LANDING (DOOR JAMB) IAW EA 8-5310-T0347719 PT1 FUSELAGE MAIN FRAME - AFT ENTRY ACCESS DOOR JAMB (P/N AJC7207-21) REPAIR. MAJOR REPAIR.
Part: SKIN — CRACKED (TE FLAP) · airframe 73,749 hrs · 25,227 cycles
RT WING OUTBD FLAP UPPER SURFACE HAS CRACKS RUNNING BETWEEN RIVETS AND HAS NUMEROUS LOOSE RIVETS. INSTALLED 8 BEARING STRIPS IAW SRM 51-31-01 VOL II. REMOVED DAMAGED AREA IAW SRM 57-10-00 VOL I FIG 65. L=5.80 W= 0.800. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 VOL I FIG 65. TITLE: WINGS - PLATES AND SKINS - RSC TRACKING RT WING OUTBD FLAP ACCOMPLISHED RSC TRACKING EA 8-5730-T0348058 PT1. MAJOR REPAIR.
Part: RIB — DAMAGED (INLET DUCT) · airframe 73,749 hrs · 25,227 cycles
NR 2 ENG INLET DUCT THRU PANEL 361JL HAS BROKEN PIECE OF RIB REMOVED AND REPLACED BROKEN SECTION OF RIB IAW SRM 54-10-00 VOL 1 AND DWG AJC7173. ADDED NEW REPAIR SPLICE IAW SRM 54-10-00 VOL 1. MAJOR REPAIR.
Part: WEB — CORRODED (BS 919-939) · corrosion level 2 · airframe 73,749 hrs · 25,227 cycles
MCD FLOOR SUPPORT WEB FROM STA. 919- 939 BETWEEN X75.5 AND X107.25 HAS EXFOLIATING CORROSION. REMOVED SUPPORT WEB IAW SRM 51-31-01, RECEIVED NEW SUPPORT WEB VIA VT MAE TRAVLER # T19/1424303, INSTALLED NEW SUPPORT WEB AT STA 919- 939 BETWEEN X75.25 AND 107.25 IAW SRM 51-31-01.PART MARKED IAW GMM 7-0-1001, CORROSION ON SUPPORT WEB 100% MATERIAL LOSS, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1A VOL.1. MAJOR REPAIR.
Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 73,749 hrs · 25,227 cycles
R/H WING INBD FLAP LOWER SURFACE HAS DENT WITH GOUGE. REMOVED DAMAGE AND CHECKED FOR LIMIT, FOUND TO BE OUT OF LIMIT IAW SRM 57-00-01. TRIMED OUT DAMAGE / CUT OUT DAMAGE AND FABRICATED DOUBLER. INSTALLED DOUBLER IAW SRM 51-31-01 AND 57-00-01.AT I/B FLAP LWR SKIN W.S 147 TO W.S 153.
Part: SEAT TRACK — CORRODED (BS 1239-1259) · corrosion level 2 · airframe 73,749 hrs · 25,227 cycles
MAIN CABIN SEAT TRACK RBL 8.5 F/S 1239- 1259 CORRODED. REMOVED CORROSION ON SEAT TRACK AT STA 1239-1259 RBL 8.5 IAW SRM 53-70-00 FIG 5 SHEET 2, VOL 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5, VOL 1. REMOVED AND REPLACED SEAT TRACK AT STA 1129-1269 RBL 8.5 IAW SRM 53-70-00 FIG 1, VOL 1 AND DWG NEA6022. MAJOR REPAIR.
Part: SKIN — CRACKED (RT WING) · airframe 73,749 hrs · 25,227 cycles
DURING ACCOMPLISHMENT OF EO 9-5730-E0317303 P4, FOUND A CRACK IN THE RH WING LOWER L/E SKIN AT FWD I/B CORNER OF REFUELING DOOR CUT-OUT. REPAIR PER SRM 57-10- 00, REPAIR 100, FIG. 106. DOT # 53-01 REMOVED DAMAGE ON RH LOWER LEADING EDGE SKIN AT FWD LOWER LEADING EDGE SKIN, FWD CORNER OF REFUELING DOOR CUT OUT AT STA XOS605 IAW SRM 57-10-00 VOL I. FABRICATED FILLER AND DOUBLER AND REPAIRED IAW SRM 57-10-00 FIG 107 VOL I. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 1179-1381) · corrosion level 2 · airframe 73,749 hrs · 25,227 cycles
CORROSION AT CABIN FLOOR STRUCTURE (SIDE FLANGE OF SEAT TRACK) STA 1179 TO STA 1381. X68. REMOVED CORROSION ON SEAT TRACK X68 SIDE FLANGE IAW SRM 53-70-00 FIG 5. CHECKED LIMITS, MINIMUM THICKNESS IS 0.060 AFTER REWORK MATERIAL LOSS IS 0.040. FOUND OUT OF LIMITS IAW SRM 53-70-00 FIG 5. TR14402. INSTALLED NEW SEAT TRACK PART NUMBER 60- 10964. REMOVED AND INSTALLED SEAT TRACK IAW SRM 51-31-01. (REPAIRED SEAT TRACK AT STA 1139 TO 1391. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (BS 1421-1481) · corrosion level 2 · airframe 73,749 hrs · 25,227 cycles
MAIN CABIN SEAT TRACK CORRODED F/S 1421-1481 LBL 75.25 (EXFOLIATED). REMOVED CORROSION ON SEAT TRACK FLANGE LBL 75.25 IAW SRM 53-70-00 FIG 5. CHECKED LIMITS, MINIMUM THICKNESS IS 0.060 AFTER REWORK MATERIAL LOSS IS 0.045 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. TR14402. INSTALLED NEW SEAT TRACK IAW SRM 53-70- 00 PART NUMBER AEA7325-9. (NEW SEAT TRACK INSTALLED STA 1391-1531 IAW SRM 53-70-00) MAJOR REPAIR
Part: SEAT TRACK — CORRODED (BS 1391-1531) · corrosion level 2 · airframe 73,749 hrs · 25,227 cycles
MAIN CABIN SEAT TRACK CORRODED F/S 1421-1481 LBL 75.25 (EXFOLIATED). REMOVED CORROSION ON SEAT TRACK FLANGE LBL 75.25 IAW SRM 53-70-00 FIG 5. CHECKED LIMITS, MINIMUM IS 0.060 AFTER REWORK MATERIAL LOSS IS 0.045 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. TR14402. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 PART NUMBER AEA7325-9. (NEW SEAT TRACK INSTALLED STA 1391-1531 IAW SRM 53-70-00)
Part: SEAT TRACK — GOUGED (BS 1119-1139) · airframe 73,749 hrs · 25,227 cycles
MAIN DECK R/H FLOOR SEAT TRACK# -47.50 HAS 3EA GOUGES FROM STA 1119-1139. BLENDED 3EA GOUGES IAW SRM 53-70-00. CHECKED LIMITS OF GOUGES. STA 1139 L=1.5, W=.470 D=.110 FOUND OUT OF LIMITS IAW SRM 53-70-00 (TR88614). INSTALLED NEW SEAT TRACK P/N 60-10964, BATCH# 2064395 IAW SRM 53-70-00 FIG 2. MAJOR REPAIR REWORK NON ROUTINE GENERATED TO CORRECT DOCUMENTATION ERRORS. SEE N00957 WORK ORDER 00074193 , CORRECT PART NUMBER OF SEAT TRACK IS AEA7325-17. LOCATION OF REPAIR IS STA 1129-1225 AT -X47.55. INSTALLATION REFERENCES USED DWG AEA7325 AND SRM 51-31-01 VOL II.
Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 73,330 hrs · 25,029 cycles
EMER LT TEST BUTTON PUSHED THROUGH PANEL RESECURED EMER TEST PUSH BUTTON INTO PANEL
Part: GIRT BAR — UNSECURE (DOOR) · airframe 73,296 hrs · 25,012 cycles
ON BLOCK IN DOORS WERE DISARMED HOWEVER GIRT BAR IS HANGING LOOSE ON THE FORWARD SIDE OF LEFT DOOR. REINSTALLED GIRT BAR. OPS CHECKS NORMAL REF AMM 25-61-02-4.
2018
Part: TRANSFER VALVE — FAILED (FUEL SYSTEM) · airframe 72,516 hrs · 24,637 cycles
AT FL360, A TANK 3 PUMPS OFF LEVEL 1 INDICATION, FOLLOWED BY TANK 3 TIP TRAPPED. THEN TANK 3 QTY LOW LEVEL 1 INDICATION. SWITCH AT FUEL CONTROLLER, NO HELP. REMOVED AND REPLACED THE TRANSFER VALVE IWW MM 28-21-09-2, REMOVED AND REPLACED THE TRANSFER SHUT-OFF VALVE IAW 28-21-12-2, REMOVED AND REPLACED THE FUEL FLOAT IAW MM 28-42-01-2, REMOVED AND REPLACED THE TRANSFER FLOAT VALVE IAW 28-21-10-2, OPS CHECKED IAW MM 28-14-00, OPS CHECKED GOOD.
Part: ELBOW — MALFUNCTIONED (FUEL) · airframe 71,945 hrs · 24,348 cycles
ON APPROACH, PASSING 2000 FT, LEVEL 2 LAT FUEL IMBALANCE, FUEL SHOWED 8500 , 6000 , 4500 . APPROACH CONTINUED, IMBALANCE BECAME WORSE , LANDED WITH APPROXIMATELY 9000, 6000, 4000 . AFTER SHUTTING DOWN OF THE ENGINES , AND STARTING APU , FUEL BEGAN TO BALANCE. R & R FUEL DUMP ELBOW LINE IAW AMM 28-00-01-2, AND FUEL VALVE IAW AMM 28-21-08-2. PERFORMED A FINAL LEAK CHECK IAW AMM 28-00-00-2, NO LEAKS NOTED. MAINTS ALSO PERFORMED A FUEL QUANTITY INDICATION SYSTEM TEST IAW AMM 28-41-00-5. TESTED GOOD. TROUBLESHOT LATERAL FUEL UNBALANCE FAULTS IAW FIM 28-14-00-810-805. NO FAULTS FOUND.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,863 hrs · 24,306 cycles
ACFT FAILED AN EMERGENCY LIGHT TEST. RECEIVED A LVL 1 EMERGENCY BATTERY 1 LOW ALERT DURING TEST. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED NORMAL, OK FOR SERVICE.
2017
Part: STRUT — LEAKING (MLG) · airframe 71,213 hrs · 23,961 cycles
CENTER MLG STRUT HAS RUNNING LEAK WITH STRUT PRESSURE AT 0 PSI. CTR GEAR RETRACTED. DO NOT OPERATE CTR GEAR. REMOVED THE CENTER GEAR STRUT AND FOUND STRUT DAMAGE. R&R THE CENTER MLG GEAR.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,980 hrs · 23,837 cycles
CENTER CARGO FLOORBEAM CRACKED 2 PLACES AT STATION 1741. FLOORBEAM REPAIR C/W REF EA 8-5310-T0335263.
Part: FRAME — DAMAGED (LT MLG) · airframe 70,508 hrs · 23,608 cycles
LEFT MLG RETRACT ACTUATOR A-FRAME ATTACH FITTING AFT BUSHING LOOSE. REPAIRED AIRFRAME IAW EA 8-5740-T0333341. FOUND CORROSION INSIDE A-FRAME ACTUATOR RETRACT. HONNED A-FRAME BORE TO 2.265 TO REMOVE CORROSION. REPAIRED THE FRAME IAW EA. 8-5740-T0333341 P1.
Part: WEB — CRACKED (BS 1841) · airframe 70,505 hrs · 23,607 cycles
CENTER CARGO COMPARTMENT BILGE AREA THE WEB CRACKED AT BS 1841, RBL 33. REMOVED AND REPLACED THE WEB IAW DRAWING AGA7170.
Part: WEB — CRACKED (BS 1841) · airframe 70,505 hrs · 23,607 cycles
CENTER CARGO COMPARTMENT BILGE AREA AT BS 1841, RBL 46 CRACKED ON WEB. REMOVED AND REPLACED THE WEB IAW DRAWING AGA7170.
Part: ACCESS PANEL — CRACKED (NR 2 NACELLE) · airframe 70,505 hrs · 23,607 cycles
NR 2 ENGINE PYLON ACCESS PANEL 457CT SKIN CRACKED AT YID 425.30. REPAIRED THE ACCESS PANEL IAW EA 8-5480-T0333228.
Part: BEAM — CRACKED (R3 DOOR PLUG) · airframe 70,505 hrs · 23,607 cycles
MAIN CABIN R3 PLUG DOOR UPPER FRAME IS DAMAGED. REMOVED AND REPLACED THE UPPER BEAM AT THE R3 PLUG DOOR IAW DWG ADA3462.
Part: SUPPORT BRACKET — CRACKED (BS 1246) · airframe 70,505 hrs · 23,607 cycles
LOWER FUSELAGE LEFT SIDE, BS 1246, FWD OF FILLET PANEL 151ET, HAS SUPPORT BRACKET CRACKED. REMOVED AND REPLACED THE BRACKET IAW DWG ANB7102.
Part: SKIN — DAMAGED (RUDDER) · airframe 70,505 hrs · 23,607 cycles
MINOR DAMAGE AT THE TOP LEFT OF LOWER RUDDER. TRIMMED OUT DAMAGE AND INSTALLED A DOUBLER IAW SRM 55-00-01, FIG 3, SHEET 2.
Part: FLOOR SUPPORT — CORRODED (BS 422) · airframe 70,505 hrs · 23,607 cycles
MAIN CABIN BS 422, LONGERON 27R, UNDER FLOOR SUPPORT CORRODED. REMOVED AND REPLACED CHANNEL FLOOR SUPPORT IAW DWGS ABA 7338 & NBA 6018 AND SRM 51-31-01, VOL 2.
Part: FLOORBEAM — CORRODED (BS 1841) · corrosion level 2 · airframe 70,505 hrs · 23,607 cycles
CENTER CARGO BAY BILGE AREA AT BS 1841 HAS CORROSION ALONG THE FLOORBEAM. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FIG 7, SHEET 2, VOLUME 1, AND EA 8-5310-T0333280.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,505 hrs · 23,607 cycles
AFT CARGO COMPT, LT SEAT TRACK HAS (2) AREAS OF EXFOLIATION CORROSION ON THE UNDERSIDE FROM STA 1921-1967. REPAIRED CORRODED SEAT TRACK IN BOTH AREAS FROM STATION 1921 TO STATION 1967 REF SRM 53-70-00 FIG 18 VOL 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 70,505 hrs · 23,607 cycles
MAIN CARGO COMPT, APPROX STA 1381-1401 X= 8.50, TWO SEAT TRACK LOBES GOUGED. REPLACED SECTION DAMAGED OF SEAT TRACK FROM STA 1381 TO 1471, LBL 8.5 REF SRM 53-70-00 FIG 1, SHEET 1, VOL 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 70,505 hrs · 23,607 cycles
MAIN CARGO COMPT, APPROX STA 1501-1521 X = -47.50, TWO SEAT TRACK LOBES GOUGED. REPLACED SECTION DAMAGED OF SEAT TRACK FROM STA 1471 TO 1551, RBL 47.5 REF SRM 53-70-00 FIG 1, SHEET 1, VOL 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 70,505 hrs · 23,607 cycles
MAIN CARGO COMPT, APPROX STA 1501-1521 X= 8.50, TWO SEAT TRACK LOBES GOUGED. REPLACED SECTION DAMAGED OF SEAT TRACK FROM STA 1471 TO STA 1531, LBL 8.5 REF SRM 53-70-00 FIG 1, SHEET 1, VOL 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 70,505 hrs · 23,607 cycles
MAIN CARGO COMPT, APPROX STA 1491 X= 27.50, SEAT TRACK GOUGED. REPLACED SECTION OF DAMAGED SEAT TRACK FROM STA 1481 TO STA 1531 REF SRM 53-70-00 FIG 1, SHEET 1, VOL 1.
Part: SKIN — CRACKED (TE FLAP) · airframe 70,446 hrs · 23,582 cycles
RT I/B FLAP UPPER SKIN HAS ABOUT 4" CRACK. FABRICATED AND DRILLED SKIN FILLER AND 2 REPAIR SPLICE/DOUBLERS IN REF TO SRM 57-10-00 FIG 86. INSTALLED REPAIR SPLICES/DOUBLERS AND SKIN FILLER ON FLAP IN REF TO SRM 57-10-00 FIG 86. RESTORED EXTERIOR FINISH OF INBD FLAP REPAIR AREA REF SRM 51-21-02.
Part: WEB — CRACKED (NLG WW) · airframe 70,189 hrs · 23,471 cycles
FOUND A CRACK IN THE RT NOSE WHEEL WELL SUPPORT WEB. INSTALLED PERMENANT DOUBLER REPAIR IAW SRM 53-30-00, PAR 8, FIGURE 6, SHEET 2.
2016
Part: DUCT — ODOR (AC SYSTEM) · airframe 69,696 hrs · 23,266 cycles
FUME EVENT AFTER TURNING ON THE PACKS FOR THIS FLIGHT. APU WAS AIR SOURCE. NO SMELL IN FLIGHT. PERFORMED A/C PACK DISTRIBUTION DUCT ODOR CLEANING PER MM 21-53-00-7. AFTER RUNNING PACK IN HIGH FOR 15, HAD NO FUMES SMELL IN COCKPIT, FOUND NO OIL LEAKING ON APU AIR DUCT A/C OK FOR SERVICE.
Part: FAIRING — DAMAGED · airframe 69,285 hrs · 23,073 cycles
POST FLIGHT FOUND DAMAGE ON TRAILING EGDE OF AFT UPPER FAIRING LT SIDE. R & R MULTIPLE LOOSE FASTENERS ON BOAT TAIL IN REF TO SRM 51-30-00 VOL 2. SEALED T/E IN REF TO 51-41-01, VOL 2.
Part: COMPUTER — FAILED (COCKPIT) · airframe 69,010 hrs · 22,956 cycles
LEVEL 3 CABIN SMOKE ALERT AT GATE WITH MX PRESENT, NUMEROUS INTERMITTENT. REPEAT WRITE UP. REMOVED & REPLACED MSC PER AMM 31-42-01-4-0. RAN APU & ENGINE SUPPLIED AIRLOAD SYSTEM CHECKS GOOD IN REF WITH JRH. INSPECTED & CLEANED CAC OF WATER REF SMP.
2015
Part: OXYGEN MASK — NOT SEATED (COCKPIT) · airframe 68,053 hrs · 22,549 cycles
NOTED OXYGEN QTY AT OR NEAR 0 ON ALL 4 SYSTEMS AFTER LANDING CHECK, NORMAL RANGE DURING PRE-FLIGHT. UPON PRESSURIZING THE O2 SYS, FOUND NR 2 JUMP SEAT OXYGEN MASK WAS LEAKING. RESEATED & STOWED O2 MASK PROPERLY & LEAK CHECKED GOOD. NEED TO REPLACE BOTH NR 1 & 2 OXYGEN BOTTLES, HAVE ONE IN STOCK & REPLACED SAME IAW AMM 35-11-01-4. WAITING FOR 2ND BOTTLE ARRIVAL. REPLACED BOTH NR 1 & 2 OXYGEN BOTTLES IAW AMM 35-11-01-4, LEAK CHECKED GOOD. NR 3 & 4 O2 BOTTLES DEFERRED, SEE WRI 35-10 2224.
Part: SENSOR — FAILED (NR 2 ENGINE) · airframe 679 hrs · 22,510 cycles
REJECTED TAKEOFF FOR ENG FAIL LIGHT AT 90 KTS. FOLLOWING REJECT, ALL ENG INDICATIONS APPEARED NORMAL. NO INDICATION OF WHICH ENG CAUSED THE ENG FAIL LIGHT. R & R NR 2 ENG FAN SENSOR POSITION 2 IAW AMM 71-11-01-2. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: GIRT BAR — MISSING (ZONE 800) · airframe 67,888 hrs · 22,483 cycles
L1 DOOR GIRT BAR MISSING. ACFT INDUCTED INTO B CHECK ON 11 12 15. DURING THE L1 DOOR INSPECTION, THE L1 DOOR GIRT BAR WAS FOUND MISSING PART HAS BEEN PLACED WITH AOG, PN ABA7949-503, MSN 1568334 ONCE RECEIVED. FLIGHT 1533 NOV 3 2015 NEW GIRT BAR WILL BE REINSTALLED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 673 hrs · 22,227 cycles
MAIN CABIN, RT APPROX STATION 1800 RBL 48 SEAT TRACK EXFOLIATED. R & R DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 1.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 673 hrs · 22,227 cycles
MAIN DECK SEAT TRACK LOB DAMAGED AT STATION 1380, RBL 12". REPLACED DAMAGED SECTION OF SEAT TRACK ON MAIN DECK AT STATION 1380, RBL 12". BY SPLICING IN NEW SECTION IAW SRM 53-70-01 VOL I.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 673 hrs · 22,227 cycles
MAIN DECK SEAT TRACK LOB DAMAGED AT STATION 1821, LBL 51". REMOVED SECTION OF DAMAGED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 VOL 1.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 673 hrs · 22,227 cycles
MAIN CABIN, DAMAGED SEAT TRACK AT APPROX STATION 1255, LBL 72. REMOVED DAMAGED SEAT TRACK FROM STATION 1249 - 1371, LBL 48. REPLACED SEAT TRACK AS REQUIRED IAW SRM 53.70.00 VOL I.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 673 hrs · 22,227 cycles
MAIN DECK SEAT TRACK LOB DAMAGED AT STATION 1640, LBL 51. REPAIRED SEAT TRACK IAW SRM 53-70-00.
Part: BEAM — CRACKED (L3 DOOR) · airframe 673 hrs · 22,227 cycles
MAIN CABIN, L3 DOOR IS CRACKED AT UPPER FWD FRAME. R & R BEAM ADA0006-1 IAW DWG ADA3462 & SRM 51-31-01.
Part: COALESCER BAG — DIRTY (ZONE 100) · airframe 671 hrs · 22,146 cycles
MODERATE FUEL & OIL ODOR EMANATING FROM NR 1 PACK. SELECTED OFF DUE TO SMELL. RAN NR 1 PACK WITH APU PNEUMATICS. NO FUEL OR OIL ODOR. CHECKED 30 DAY HISTORY FOR ATA 21, NO RELATED HISTORY. R & R NR 1 COALESCER BAG. BAG WAS FILTHY BUT NO FUEL OR OIL ODOR ON BAG OR INSIDE WATER SEPARATOR HOUSING IAW AMM 21-54-03-2. LEAK CHECKED GOOD. HAD LEAD AMT RUN NR 1 ENG IAW JRH CHAPTER 5 & RAN NR 1 PACK WITH ENG PNEUMATICS. NO FUEL OR OIL ODOR FROM NR 1 PACK IAW AMM 21-00-01-5. ACFT OK FOR SERVICE.
Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 669 hrs · 22,047 cycles
LI SLIDE PRESS WILL NOT CHECK ON PREFLIGHT. LIGHT WILL NOT ILLUMINATE. R & R BATTERIES FOR LT DOOR SLIDE & CHECKED OK.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 667 hrs · 21,990 cycles
LEFT AFT PACK EXHAUST VLV CUT OUT HAS A CRACK IN THE UPPER AFT CORNER. REPAIRED CRACK IAW SRM CH 53-50-00.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 667 hrs · 21,990 cycles
NUMBER 3 PACK DOOR CUT OUT HAS A CRACK IN THE AFT UPPER CORNER. REPAIRED CRACK IAW SRM 53-50-00.
2011
Part: FEEDER CABLE — BURNED (NR 3 NACELLE) · airframe 61,183 hrs · 19,628 cycles
DURING C-CHECK, NR 3 ENGINE PYLON, POWER FEEDER CABLE ONE PHASE IS ARCING AND BURNING THRU STRUCTURAL MEMBER BELOW PRECOOLER PLENUM ASSY BETWEEN APPROX YN 259 AND YN 268. R & R NR 3 ENG PYLON POWER FEEDER CABLE IAW EO 8-2450-7-5009 PT2.
2010
Part: ENGINE — FAILED (ZONE 400) · airframe 57,545 hrs · 18,272 cycles
TEST FLIGHT-UNABLE TO RESTART NR 1 ENGINE AIRBORNE AFTER SHUTDOWN WHEN FUEL LEVER SELECTED ON N1 INDICATION WENT TO "0", AFTER 20 SECS, WHEN FUEL LEVER SELECTED OFF, N1 INDICATION CAME BACK AFTER 15-20 SECS, START ATTEMPT WAS AT FL 240- 250, 240 KNOTS-280 KNOTS-NEVER HAD EGT RISE. R & R NR 1 MCD IAW AMM 73-20-01-2, ENG FAILS TEST, R & R NR 1 ENG IAW WORKCARD 71T0101-1, LEAKS AND OPS CKD GOOD ON NR 1 ENGINE IAW AMM AND JRH, NO DEFECT NOTED, MINOR REPAIR.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 57,541 hrs · 18,267 cycles
MAIN CARGO AREA, SEAT TRACK, APPROX STA 1089 AT RBL 28 IS CRACKED UNDER HANDLING SYS BRACKET. R & R MCD SEAT TRACK SEGMENT FROM FS 1045 TO FS 1125 AT RBL28 IAW SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1491) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK AT FS 1491 HAS 1 EACH WORN LOBE AT RBL 47.5. REMOVED AND REPLACED SEAT TRACK IAW SRM 57-70-00 AND SRM 51-31-01, SEAT TRACK FABRICATED ON MAE TRAVELER NR T10/815830 IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.
Part: STOP FITTING — BROKEN (L3 DOOR) · airframe 57,541 hrs · 18,267 cycles
MCD L-3 DOOR PLUG LOWER FWD STOP FITTING BROKEN. REMOVED AND REPLACED L-3 DOOR PLUG LOWER BEAM FITTING IAW SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1301) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK AT FS 1301 AT RBL 47.5 HAS 1 EACH WORN LOBE. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 AND SRM 51-31-01, SEAT TRACK FABRICATED ON MAE TRAVELLER NR T10/817056, T10/817057 IAW SRM 53-70-00 AND SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 979-1085) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT. SEAT TRACK BETWEEN F.S. 979 TO FS 1085 AT RBL 47.5 HAVE 8 EACH WORN LUGS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1179-1311) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT. SEAT TRACK BETWEEN FS 1179 TO FS 1311 AT LBL 47.5 HAVE 5 EACH WORN LOBES. REPAIRED SEAT TRACK AND FOUND WITHIN LIMITS IAW SRM 57-70-00 FIG. 5, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AND SRM 57-70-00 FIG 5, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1015-1159) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMP SEAT TRACK BETWEEN F.S. 1015 TO F.S. 1159 AT LBL 47.5 HAVE 8 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 1015 TO FS 1159 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR, SEAT TRACK SECTION FABRICATED ON MAE TRAVELLER NR T10/817049 IAW SRM 51-10-01.
Part: SEAT TRACK — WORN (BS 1511-1521) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK BETWEEN F.S. 1511 TO F.S. 1521 HAS 2 EACH WORN LOBES AT LBL 8. MCD CARGO COMPT SEAT TRACK BETWEEN FS 1511 TO FS 1521 AT LBL 8 HAS BEEN REPLACED ON NON-ROUTINE NR N00389 IAW SRM 53-70-00 SHEET 1 AND 2, SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 879-1019) · airframe 57,541 hrs · 18,267 cycles
UPPER CARGO COMPARTMENT SEAT TRACK LBL 47.5. FS 1019 TO 879 HAS 3 EA WORN LOBES- OUT OF LIMITS. R & R SEAT TRACK SECTION IAW SRM 53-70-00, STA. 869 TO STA 1009 LBL 47.5. SEAT TRACK SECTION FABRICATED ON MAE TRAVELER T10/816283. REPAIR CLASSIFIED AS MAJOR REPAIR.
Part: SKIN — CHAFED (ZONE 100) · airframe 57,541 hrs · 18,267 cycles
FUSELAGE EXTERNAL SKIN IS CHAFED AND GOUGED AT LWR CTR CARGO DOOR LWR AFT JAMB BELOW SEAL RETAINER. REPAIRED FUSELAGE EXTERNAL SKIN AT CTR CARGO DOOR LOWER AFT JAMB BELOW SEAL RETAINER IAW SRM 53-50-00.MAJOR REPAIR.
Part: SEAT TRACK — WORN (BS 795) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK AT FS 795 HAS 1 EACH WORN LUG AT RBL 47.5. REMOVED AND REPLACED SEAT TRACK IAW SRM 57-70-00 AND SRM 51-31-01, SEAT TRACK FABRICATED IAW SRM 53-42-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1431-1531) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK BETWEEN FS 1431 TO FS 1531 AT LBL 47.5 HAS 6 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK BETWEEN F.S. 1431 TO F.S. 1531 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT. SEAT TRACK BETWEEN FS 1159 TO FS 1259 AT LBL 27.5 HAS 4 EACH WORN LOBES. BLENDED SEAT TRACK AND FOUND OUT OF LIMIT AT STA 1249, REMOVED AND REPLACED SEAT TRACK BETWEEN STA 1239 TO STA 1259 AT LBL 27.5 IAW SRM 51-31-01 AND SRM 53-70-00, SEAT TRACK FABRICATED IAW SRM 51-10-01, SEAT TRACK BETWEEN FS 1159 TO 1248 FOUND WITHIN LIMIT AFTER BLENDING IAW SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 1431-1531) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT. SEAT TRACK BETWEEN F.S. 1431 TO F.S. 1531 AT LBL 47.5 HAVE 6 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK FROM F.S. 1431 TO F.S. 1531 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, CLASSIED AS MAJOR REPAIR.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT. SEAT TRACK AT FS 1391 AT LBL8 HAS 1 EACH WORN LOBE. REMOVED SEAT TRACK IAW SRM 51-31-01, FABRICATED NEW SEAT TRACK IAW SRM 53-42-01 AND SRM 51-00-00-1, INSTALLED SEAT TRACK IAW SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — WORN (BS 635) · airframe 57,541 hrs · 18,267 cycles
MCD CARGO COMPT SEAT TRACK AT FS 635 AT LBL 47.5 HAS 1 EACH WORN LOBE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AND SRM 57-70-00, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 57,541 hrs · 18,267 cycles
UPPER CARGO COMPARTMENT BL100R TRACK RAIL, F.S. 745 TO 765 HAS 3 EACH CHAFE MARKS. SEAT TRACK CHAFING MARKS OUT OF LIMITS IAW SRM 53-70-00 FIG.5 MATL LOSS 0.10 AFTER CLEAN-UP. REMOVED SEAT TRACK AND 4EA. FLOOR SUPPORTS FROM STATION 635 TO FS 795, RBL 100 IAW SRM 51-31-01. FABRICATED NEW SEAT TRACK PN TMS60-19943, LOCATED AND DRILLED IAW SRM 53-70-00 AND SRM 51-31-01. INSTALLED NEW SEAT TRACK AND 4 EA FLOOR SUPPORTS IAW SRM 53-70-00 AND SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR REPAIR.
2009
Part: TRANSCOWL — DEPARTED (THRUST REVERSER) · airframe 56,720 hrs · 17,987 cycles
TOWER INFORMED US WE DROPPED SOMETHING ON ROLLOUT. SMOOTH LANDING, REVERSERS STOWED BY 65-70KTS. A LARGE PIECE OF NR 2 REVERSER CAME OFF AT END OF LANDING, ROLL INITIALLY GOT ALL 3 ENGINES SHOWING REV STOWED THEN NR 2 U/L LIGHT CAME ON. SHUTDOWN NR 2 AND TAXIED IN. NO OTHER INDICATIONS NOTED. THE NR 2 RT TRANSCOWL FELL OFF ACFT DURING REVERSE ACTIVATION ON LANDING. REMOVED AND REPLACED NR 2 ENG RT REVERSER HALF IAW WORKCARD NR 78T3701R-2. COMPLIED WITH OPS CHECK. OK FOR SERVICE.
2008
Part: SKIN — DENTED (T/E FLAP) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON LT WING INBD FLAP UPPER SKIN FOUND 2 EA DENTS: 1) UPPER 1 INCH BY 1 INCH DEEP .074 INCH 2) LWR 2 INCH BY 1.50 INCH DEEP .050 INCH. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 65.
Part: BEAM — CRACKED (ZONE 200) · airframe 53,453 hrs · 16,870 cycles
FWD CARGO COMPT PERFORMED REWORKING IAW EO 8-2550-7-2354 P1 ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL I.
Part: SKIN — CRACKED (TE FLAPS) · airframe 53,453 hrs · 16,870 cycles
LT WING INBOARD FLAP ON UPPER SKIN FOUND SCRATCH.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 53,453 hrs · 16,870 cycles
LT WING INBOARD FLAP ON UPPER SKIN FOUND CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.
Part: BEAM — CRACKED (ZONE 200) · airframe 53,453 hrs · 16,870 cycles
CTR CARGO COMPT ON BEAM FOUND CRACK 0.70" LONG. REPAIRED BEAM IAW SRM 53-00-01 VOL I FIG 4 SHT 2.
Part: SKIN — WORN (ZONE 600) · airframe 53,453 hrs · 16,870 cycles
RT WING LWR SIDE EXT ZONE FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 36 AND 39 VOL I.
Part: FRAME — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AFT FUSE WASTE TANK COMPT ON FRAME FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 FIG 4 VOL I.
Part: SKIN — DENTED (RT ELEVATOR) · airframe 53,453 hrs · 16,870 cycles
RT INBD ELEVATOR LWR SURFACE FOUND DENT ON SKIN.
Part: SKIN — DENTED (RT ELEVATOR) · airframe 53,453 hrs · 16,870 cycles
RT INBD ELEVATOR LWR SURFACE FOUND DENT ON SKIN. REPAIRED AREA IAW SRM 51-10-00 FIG 8 VOL I.
2007
Part: SKIN — DENTED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
EXT FUSELAGE LWR SKIN FOUND 2 DEEP DENT, 1) 6 INCH BY 2 INCH THE WIDTH OF THE DENT IS APPROX .09 INCH, 2) 7 INCH BY 2 INCH THE WIDTH OF THE DENT IS APPROX .09 INCH. REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHT 2A VOL I.
Part: SKIN — DENTED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
EXT FUSELAGE LWR SKIN FOUND 2 EA DEEP DENT: 6 INCH BY 2" THE WIDTH OF THE DENT IS APPROX .09", 7" BY 2" THE WIDTH OF THE DENT IS APPROX 09".
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
CTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
CTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
CTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1-2 VOL I.
Part: SKIN — CRACKED (LT ELEVATOR) · airframe 53,453 hrs · 16,870 cycles
LT INBD ELEVATOR OUTER RIB UPPER SKIN WITH .25 INCH CRACK. REPAIRED SKIN IAW SRM 55-10-00 FIG 8 VOL I.
Part: SKIN — CRACKED (LT ELEVATOR) · airframe 53,453 hrs · 16,870 cycles
LT INBD ELEVATOR OUTER RIB WITH 1/4" CRACK ON RIB AND LOWER SKIN.
Part: SKIN — CRACKED (LT ELEVATOR) · airframe 53,453 hrs · 16,870 cycles
LT INBD ELEVATOR OUTER RIB WITH 1/4 INCH CRACK ON RIB AND LOWER SKIN. REPAIRED AREA IAW SRM 55-10-00 FIG 8 VOL I.
Part: STIFFENER — WORN (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT LT SIDE ON VERTICAL BULKHEAD ON NR 2 VERT STIFFENER FOUND DEEP WEAR.
Part: STIFFENER — WORN (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT LT SIDE ON VERTICAL BHD ON NR 2 VERT STIFFENER FOUND DEEP WEAR. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 8 AND 9.
Part: SKIN — DENTED (ZONE 600) · airframe 53,453 hrs · 16,870 cycles
RT WING L/E DURING INSPECTION REPAIR ASSESMENT FOUND NR 3 DENTS ON EXT SKIN, 1.5" BY 1.5" DEEP .09", 1" BY 1.5" DEEP .04",BY 1" BY 1" DEEP .07". REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 40.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
AFT CARGO COMPT SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED SEAT TRACK SECTION IAW SRM 53-70-00 VOL I FIG 1.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 53,453 hrs · 16,870 cycles
MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
MAIN CABIN ENTRY WAY SEVERE CORROSION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 53,453 hrs · 16,870 cycles
MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 53,453 hrs · 16,870 cycles
MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 57-70-00 FIG 1 VOL I.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,453 hrs · 16,870 cycles
MAIN CABIN ENTRY WAY SEVERE CORROSION ON SEAT TRACK.
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT LT SIDE ON VERTICAL BHD FOUND CRACK.
Part: BULKHEAD — CRACKED (BS 485) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT LT SIDE ON VERTICAL BULKHEAD FOUND CRACK. REPAIRED AREA IAW SRM 53-40-00 FIG 34 VOL I.
Part: FRAME — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
FWD AVIONICS COMPT ON FRAME FOUND CRACK.
Part: FRAME — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT RT SIDE ON FRAME JAMB DOOR FOUND CRACK.
Part: FRAME — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
FWD AVIONICS COMPT ON FRAME FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 FIG 11 VOL I.
Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 53,453 hrs · 16,870 cycles
AIR CONDITIONING COMPT RT SIDE ON FRAME JAMB DOOR FOUND CRACK. REPAIRED AREA IAW SRM 53-00-01 FIG 8 VOL I.
Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 53,453 hrs · 16,870 cycles
DURING U/S INSP OF HORIZONTAL STAB, FOUND CRACK ON PANEL P/N 7227-1, POSITION 14, CRACK IS IN FLYABLE LIMITS, ATTACHED INSPECTION FINDING FORM FOR A11 DETAIL. REPAIRED AREA IAW EA 8-5510-111537.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,453 hrs · 16,870 cycles
DURING VISUAL INSP OF HORIZONTAL STAB SKIN PANEL INSPECTION, FOUND CRACK ON PANEL P/N 7439-2 SERIES -10, REPAIRED AREA IAW EA# 8-5510-111620.
Part: SKIN — LOOSE (LT WING TE FLAP) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON LT WING OTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.
Part: SKIN — LOOSE (ZONE 500) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON LT WING OUTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS.
Part: SKIN — LOOSE (ZONE 500) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON LT WING OTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.
Part: SKIN — LOOSE (ZONE 500) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON LT WING OUTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS.
Part: SKIN — LOOSE (ZONE 600) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON RT WING OTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS. REPAIRED AREA IAW SRM 57-00-01 VOL I FIG 4 SHT 5.
Part: SKIN — LOOSE (ZONE 600) · airframe 53,453 hrs · 16,870 cycles
DURING INSPECTION ON RT WING OUTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS.
2006
Part: SKIN — GOUGED (WING) · airframe 52,082 hrs · 16,256 cycles
LWR SURFACE OF WING JUST O/B OF AFT PYLON HAS DEEP GAUGE FROM DEPARTURE OF PYLON "V" PANEL DURING FLIGHT NR 3 PYLON. GOUGE LOCATION ON RIGHT WING BOTTOM SKIN BETWEEN S41 AND S40 AT XORS 372.0. GOUGE MEASURES 5.5 IN LONG AND 0.060 DEEP AT DEEPEST POINT. GOUGE IS APPROX 0.5 IN FROM FASTENER AND PER SRM 57-00-01 PG 5 OF VOL 1. THE BLEND OUT NEEDS TO BE 30Y WITH CURRENT AREA BLEND CAN ONLY BE APPROX 10Y. CONTACTED MEM ENGR FOR EA TO BLEND AREA. AS STATED IN PREVIOUS "SHGN", ENGINEERING HAS BEEN LOOKING INTO THIS DISCREPANCY. ENG HAS FOUND EA WAS NOT NEEDED. THE SRM HAS AN APPROVED REPAIR. BLENDED DAMAGED AREA IN ACCORDANCE WITH DC-10 SRM, CHAPTER 57-10-00 VOL 1 FIG 66.
Part: VALVE — LEAKING (GALLEY) · airframe 51,102 hrs · 15,825 cycles
AFTER TAKEOFF HEARD LOUD BANG AND PRONOUNCED BURNT RUBBER SMELL IN PERMEATE FLIGHT DECK, SUSPECTED BLOWN TIRE. LOWERED GEAR AND RETURNED FOR LANDING. INSP NOSE GEAR, NOSE TIRES, AND NOSE STEERING, NOSE BRAKES, PACK COMPTS, CANS, FWD AVI COMPT ALL RACKS, CNT E AND E. NTF DURING INSP OF EXTERIOR INSP FOUND PNL AVB 7332-503 OPEN LEFT SIDE NR 2 ENG, INSP INSIDE PNL AREA, NO DEFECTS OR LOOSE ITEMS. A/C FAILED DK CHECK, NR 2 PNEUMATIC SYS. REMOVED AND REPLACED ALL THREE COALESCER BAGS. OPS CHECKED NOSE GEAR 10 TIMES, NO ABNORMAL SOUNDS NOTED AT THIS TIME. TIGHTENED UP LEAKS ON PACKS 1 & 3. REPLACED AFT CARGO GALLEY/LAV PRESS REG VALVE. OPS/LEAK CHECKS GOOD. PERFORMED SYSTEM 1, 2 & 3 DECAY CKS OK.
2004
Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 48,198 hrs · 14,782 cycles
AFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS REDUCED, THE NR 1 LIGHT EXTINGUISHED. COMPLIED WITH QRH. LIGHT REMAINED EXTINGUISHED. R AND R NR 2 ENGINE FUEL FILTER. R AND R NR 1 AND 3 FUEL FILTERS AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. RAN ALL THREE ENGINES LEAK CK NORMAL. RAN AT HIGH POWER PER MAX POWER ASSURANCE CHECK. NO FUEL FILTER PRESS LIGHT ON AT ANY TIME. A/C OKAY FOR FLIGHT.
Part: WARNING LIGHT — INTERMITTENT (COCKPIT) · airframe 46,630 hrs · 14,273 cycles
LEFT MAIN GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP/IN, S/O PANEL LEFT GEAR (MAIN) LIGHT WAS INTERMITTENTLY ON. COMPLETED RED TABS, ALL LIGHTS CHECKED OUT. PERFORMED SELF CHECK OF PSEU CHECK CHANNELS 8, 12, 16 AND 20, NO FAULTS NOTED AND PER DC-10-30, QRH 2-6-2-6, OPS CHECK GOOD IAW DC-10-30 TAFI 32-30-00.
2003
Part: BEAM — CORRODED (RT MLG WW) · corrosion level 2 · airframe 43,440 hrs · 13,258 cycles
TEE CAP AEA 7097-1, STA.1521 WAS FOUND CORRODED AT RT STA.-80.125 WHERE VERTICLE BEAM A0024-2 ATTACHES. THE BEAM ATTCHMENT TO THE TEE CAP CREATES A (V) WHERE WATER CAN PUDDLE. AWAITING APPROVED REPAIR FROM BOEING
2000
Part: CONTROL CABLE — DAMAGED (NR 2 THROTTLE)
DURING DESCENT, NR 2 THROTTLE STUCK AT 88 PERCENT N2. THROTTLE WILL MOVE BUT N2 REMAINS AT 88 PERCENT N2 AND THROTTLE RETURNS TO ORIG POS. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE REF MM 76-11-01-2. RIGGED PER DC-10 MM 76-11-01-2 AND SECURED ALL ROD ENDS AND SAFTIED. AC OK FOR SERVICE.
1998
Part: HOSE ASSY — BROKEN (NR 2 ENGINE)
APPROXIMATELY 20 MIN INTO FLIGHT, NR 2 HYD QUANTITY AND PRESSURE WENT TO ZERO. ENGINE RAN APPROXIMATELY 55 MINUTES BEFORE SHUTING DOWN. T/S FOUND NR 2 ENG FIRE-RESISTANT HOSE ASSY BROKEN. REPLACED NEW HOSE ASSY AND REPLACED BOTH ENG DRIVE PUMP AND FILTERS CHECKED, NO CONTAMINATION. REPLACED FILTERS AND LEAK CHK BY ENG RAN NML PER M/M 29-11-02-2, 29-12-0 2-2 ENG RAN BY 136501, 252482.