N649FE
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
No NTSB accidents or incidents on file for this aircraft.
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.
181 reports on file, 2022-01-18 – 2023-01-02.
Part: SEAT TRACK — CORRODED (BS 1841-1850) · airframe 86,982 hrs · 16,633 cycles
MAIN DECK TRACK AT APPROX STA 1841-1850 RBL 08. SEAT TRACK LOBE CORODED. INSTALLED SEAT TRACK AND SPLICE AT STA.1841-1850 RBL 08 PER SRM 53-00-52-2R FIG.201 REPAIR 2. SEALED PER SRM 51-41-01-0G. INSTALLED FASTNERS PER DWG. SR10-53-002 AND SRM 51-35-01-0G.
Part: SEAT TRACK — CORRODED (BS 1239-1256) · corrosion level 3 · airframe 86,982 hrs · 16,633 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1239 - 1256 RBL 76. INSTALLED SEAT TRACK REPAIR AT STA. 1239-1256, RBL76, PER SRM 53-00-52-2R FIG.201 SHT.1. SEALED PARTS PER SRM 51-41-01-0G, FASTNER INSTALLATION PER SRM 51-35-01-0G.
Part: SEAT TRACK — CORRODED (BS 1165 RBL 28) · airframe 86,982 hrs · 16,633 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1165 RBL 28. INSTALLED SEAT TRACK AND SPLICE AT STA 1159-1199, RBL 28 PER SRM 53-00-52-2R FIG 201. REPAIR 2. SEALED PER SRM 51-41-01-OG. INSTALLED FASTNERS PER FDX DRAWING SR10-53- 002, AND SRM 51-35-01-OG.
Earlier reports · 2022 · 178 reports
2022
Part: SEAT TRACK — CORRODED (BS 1841-1850) · airframe 86,924 hrs · 16,609 cycles
MAIN DECK TRACK AT APPROX STA 1841-1850 RBL 08. SEAT TRACK LOBE CORODED. INSTALLED SEAT TRACK AND SPLICE AT STA.1841-1850 RBL 08 PER SRM 53-00-52-2R FIG.201 REPAIR 2. SEALED PER SRM 51-41-01-0G. INSTALLED FASTNERS PER FDX DWG. SR10-53-002 AND SRM 51-35-01-0G.
Part: CARGO TRACK — CORRODED (BS 1165 RBL 28) · corrosion level 2 · airframe 86,924 hrs · 16,609 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1165 RBL 28. (MARKED #8) 0000435071 : HARPER, RICHARD R - 15-MAR-2022 20:27 INSTALLED SEAT TRACK AND SPLICE AT STA 1159-1199, RBL 28 PER SRM 53-00-52-2R FIG 201. REPAIR 2. SEALED PER SRM 51-41-01-OG. INSTALLED FASTNERS PER FDX DRAWING SR10-53- 002, AND SRM 51-35-01-OG. 0000275049 :THIS IS A UPDATE FROM SRD 22-0521 TO CHANGE CORR LEVEL FROM LEVEL 3 TO LEVEL 2
Part: SEAT TRACK — CORRODED (BS 1165) · airframe 86,924 hrs · 16,609 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1165 RBL 28. INSTALLED SEAT TRACK AND SPLICE AT STA 1159-1199, RBL 28 PER SRM 53-00-52-2R FIG 201. REPAIR 2. SEALED PER SRM 51-41-01-OG. INSTALLED FASTNERS PER FDX DRAWING SR10-53- 002, AND SRM 51-35-01-OG.
Part: CARGO TRACK — CORRODED (BS 1239-1256) · airframe 86,924 hrs · 16,609 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1239 - 1256 RBL 76. (MARKED #5) INSTALLED SEAT TRACK REPAIR AT STA. 1239-1256, RBL76, PER SRM 53-00-52-2R FIG.201 SHT.1. SEALED PARTS PER SRM 51-41-01-0G, FASTNER INSTALLATION PER SRM 51-35-01-0G. CORR LEVEL ENTERED IN ERROR. CORR LEVEL IS A LEVEL 1
Part: PUSHROD — FAILED (N/A) · airframe 86,625 hrs · 16,448 cycles
AFTER TAKEOFF NOSE GEAR DID NOT RETRACT. HAD 2 RED LIGHTS AND COULD HERE THE AIRFLOW NOISE FROM THE DOWN NOSE GEAR. DID WRY AND GOT 4 GREEN DOWN. RETURNED TO TPA AND DID NOT DECLARE AN EMERGENCY BECAUSE AFTER THE GEAR WAS DOWN ALL WAS NORMAL. DE-SERVICED AND REMOVED NLG STRUT PISTON. REMOVED NLG STRUT ORIFICE TUBE NUT AND REMOVED DIAPHRAGM TUBE REF MD-11 32-21-01-8. STILL REQUIRES STRUT SEAL INSTALLATIONS. REMOVED AND REPLACED BENT PUSHROD ON GROUND SENSING BRACKET.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- MCD ENTRY AREA- STA 695 LBL 100 FLOOR BOARD IS SPONGY. FABRICATED NEW FLOOR PANEL AT STA 695 LBL 100 (231LF) PER FEDEX DRAWING SRZ-25-005.
Part: LONGERON — CORRODED (ZONE 100) · airframe 86,555 hrs · 16,395 cycles
DURING INSTALLATION OF L3 DOOR, EXTERNAL LONGERON 28 LHS STA1289 (P/N AEA7545-1) FOUND TO HAVE EXFOLIATED CORROSION AT UPPER LEG. CORROSION REMOVED AND AREA FOUND TO BE WITHIN LIMITS PER FEDEX EA :1-5340-T0369519.
Part: FLOOR PANEL — WORN · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR PANEL STA. 1321 R/H SIDE. MISSING FLOOR BOARD. NEED TO FABRICATE FLOOR BOARD PANEL ( 262LF ) FABRICATED NEW PANEL 262LF PER DRW# SRZ-25-005
Part: NONE — NONE (N/A) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H FUSELAGE STATION 1160-1329, L46R-L48R, HAS EXISTING REPAIR FOR LIGHTNING STRIKE DAMAGE. REF. DOT #56. LIGHTENING STRIKE REPAIRED PER LUFTANSA ENG. EI-53-0241, AND SRM 53-00-01-2R-6.
Part: SPAR CAP — CRACKED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING LOWER FWD SPAR, APPROX. STA. XCW90, HAS AN EXISTING BUSHING REPAIR. DOT #55. PREVIOUSLY INSTALLED BUSHING REPAIR COMPLETED PER TAECO EI-57-0250. BOEING REF TEC-LUB-11-0060-07B
Part: CLEVIS — NONE (RT NACELLE) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H PYLON, APPROX. XORS346, AFT CLEVIS HAS PREVIOUS REWORK TO ARB7524-2. REF. DOT #57. PART WAS PREVIOUSLY TRIMMED, OK FOR SERVICE PER BOEING SERVICE REQUEST 1- 638111991-1, 1-638111991-2..
Part: SEAT TRACK — DAMAGED · airframe 86,554 hrs · 16,394 cycles
(REWORK) "NR 418 W.O. 81728 MAIN CARGO DECK, STA 445, LBL 27, SEAT TRACK BENT FROM IMPROPER LENGTH SCREW CONTACTING STRUCTURE DOT #69 (REF NR20, W/O 81728 JPF ITEM #3)" SEAT TRACK BLEND OUT OF LIMITS REF SRM 53-00-52-1A FIGURE 101. REMOVED AND REPLACED DAMAGED SEAT TRACK REF SRM 53-0052-2R, FIG. 201.
Part: SEAT TRACK — CORRODED (MAIN CARGO DECK) · airframe 86,554 hrs · 16,394 cycles
SEAT TRACK HAS CORROSION BETWEEN STATION 1461 - 1521 REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52-2R FIG 201 SHEET 1
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK FLOOR PANEL AT STA.815 RBL11 IS CORRODED. AND DAMAGED. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-05 ADA8344.
Part: PANEL — DELAMINATED (ZONE 42) · airframe 86,554 hrs · 16,394 cycles
#2 ENGINE INLET PICKLE RARREL PANEL # 361BL IS DELAMINATED . PREPPED AND REPAIRED #2 ENGINE INLET PICKLE BARREL PNL #361BL PER SRM 51-62-01- OG., DOUGLAS. DRWG.AJC7518-1
Part: SKIN — CHAFED (LT WING LE) · airframe 86,554 hrs · 16,394 cycles
L/H WING -- FIXED LEADING EDGE SKIN -- BETWEEN SLAT TRACKS 1 & 3 - "MARKED OUT OF LIMIT AREAS" FROM SLAT GOUGING WERE ERASED FROM NR 794 JPF 1 REPAIRED DAMAGED AREA REF. MD-11 SRM 57-40-02-2R FIG. 201 REPAIR 5 SHEETS 1-3, SRM 51-31-01-OG AND SRM 51-33-01-OG.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
SEAT TRACK ON MAIN DECK STATION 1715 RBL 102 CORRODED BEYOND ALLOWABLE LIMITS REPAIR PER MD 11 SRM 53-00-52-2R FIG 201
Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOORBOARD PANEL #272EF AFA8833-21 HAS DAMAGED INSERTS AFTER CLEANING PANEL FOUND LARGE CRACK . FABRICATED NEW PANEL REF FEDEX DRAWING SRZ-25-005 MAJOR REPAIR.
Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO FLOORBOARD PANEL #263FF AEA0179-32 HAS DAMAGED INSERTS FOUND MORE DAMAGE AFTER CLEANING AND INSPECTING. FABRICATED NEW PANEL REF FEDEX DRAWING SRZ-25-005 MAJOR REPAIR
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO PAMEL #AEA7727-3,262HF HAS DAMAGED INSERTS . AFTER CLEANING AND INSPECTING FOUND MORE DAMAGE TO PANEL,FABRICATED NEW PANEL REF FEDEX DRAWING SRZ-25-005 MAJOR REPAIRE
Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO FLOORBOARD PANEL #AEA0179-32 263FF HAS DAMAGED INSERTS FOUND MORE DAMAGE AFTER CLEANING AND INSPECTION , FABRICATED NEW PANEL REF FEDEX DRAWING SRZ-25-005
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #262EFHAS DAMAGE IN MULTIPLE AREAS. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 AEA7318 MAJOR REPAIR.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #283CS AT 1561-5-93 DAMAGED. FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 ADA3212.. "MAJOR REPAIR"
Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
FWD CARGO FLOOR BOARD #127EF DAMAGED FABRICATED NEW FWD CARGO FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO PANEL #AEA7727-3 ,262HF HAS DAMAGED INSERTS AFTER CLEANING PANEL AND INSPECTING FOUND MORE DAMAGE TO PANEL . FABRICATED PANELREFFEDEX DRW SRZ-25-00 MAJOR REPAIR
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD BETWEEN STA 1321-1381 HAS MUTIPLE DAMAGE AND CORRODED INSERTS. FABRICATED MAIN DECK FLOOR BOARD PANEL #263LF BETWEEN 1321-1381 . PER DRWG SRZ-25-005. MAJOR REPAIR.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL # 282DF HAS DAMAGE IN SEVERAL AREAS. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 AFA7413 , "MAJOR REPAIR"
Part: FLOORBOARD — DAMAGED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #291GF HAS DAMAGE INSERT HOLES . FABRICATED NEW MAIN DECK FLOOR BOARD PANEL PER FEDEX DRWG SRZ--25-005 AGA7972 , ' MAJOR REPAIR'
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAINDECK SEAT TRACK STA1761 LBL 8 CORROSION ON SEAT TRACK FLOOR BOARD NUT PLATE HOLES WORN BEYOND LIMITS. 0000718346 : CAWTHON, DANIEL G - 23-APR-2022 18:07 PERFORMED MAJOR REPAIR ON SEAT TRACK, INSTALLED NEW SEAT TRACK SECTION FROM STA 1731-1771 LBL8 PER SRM 53-00-52-2R REPAIR 1, SRM 51-31-01-0G, AND SRM 51-41-01-0G.
Part: SKIN — CHAFED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
R/H WING, D.L.E, UPPER SKIN, INBOARD EDGE IS CHAFED FWD OF THE ARB0296-503 RUB STRIP. ( CORRECTION: L/H DLE.) REPAIRED L/H DROOPED LEADING EDGE CHAFFED SKIN ARB2312-1, PER SRM 57-40-01-2R FIG 202/ REPAIR 15 SHT 1.
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #271HF ADA3210-13 HAS DAMAGE FABRICATED FLOORBOARD PANEL #271HF ADA3210-13 MAJOR REPAIR
Part: RIB — CRACKED (N/A) · airframe 86,554 hrs · 16,394 cycles
WING FUSELAGE FAIRING RIB RH, STA.5-113 BETWEEN STRG 28-29 - CRACK AT RIB/FUSELAGE ANGLE UPPER FASTENER. CRACK CONFIRMED USING NDT HFEC. (PANELS AFFECTED 152LT & 152KT) CUTOUT DAMAGED RIB, FABRICATED AND PROCESSED NEW REPAIR ANGLE AND SPLICE, INSTALLED NEW ANGLE AND SPLICE AT STA. 5-113 STR. 30-32 REF. MD-11 SRM 53-00-00-2R & 51- 33-01-0G. JPF ATTACHED "MAJOR REPAIR"
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOORBOARD PANEL #241AF HAS IMPACT DAMAGE AND SIGN OF DELAMINATION FABRICATED FLOORBOARD REF FEDEX DRAWING SRZ-25-005
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #241CF FOUND DISBONED DURING REMOVEL FOR INSPECTION. FABRICATE NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005, ADA8349 .
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL # 245GF HAS DELAMINATION . REPLACED WITH NEW FABRICATED FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 ADA7178.
Part: RIB — CRACKED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
RIGHT HAND INBOARD FLAP, INBOARD LEADING EDGE CAVITIE HAS A ONE INCH TEAR IN LOWER FORWARD LIGHTNING HOLE. BLENDED DAMAGE AND APPLIED DOUBLER REPAIR IAW SRM 57-00-00-2R FIG 201, SEE ALSO EA 1-5750-T0368054
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL #282GF HAS DAMAGE AND INSERTS ARE CORRODED. FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 ,AFA3200.
Part: BOLT — LOOSE (RT MLG) · airframe 86,554 hrs · 16,394 cycles
R/H MLG ACTUATOR "A" FRAME LOWER FWD ATTACH BOLT LOOSE. REMOVE AND INSTALL FITTING ASSEMBLY WITH NEW HARDWARE PER AMM 57-20-14-4.
Part: STIFFENER — CORRODED (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
CENTER WHEEL WELL LOWER AUX TANK ACCESS LANDING 143DZ FOUND 6 DOMENUTS DAMAGED. REPLACED STIFFNER REF AYB7113.
Part: NONE — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD 282JF DAMAGED. FABRICATED NEW FLOOR BOARD PANEL 282JF FEDEX DRWG SRZ-25-005 AFA4413
Part: FLOORBOARD — DELAMINATED (MAIN DECK) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK AFT FLOOR BOARD PANEL 283BS DELAM FOUND TWO LOCATION. FABRICATED NEW FLOOR BOARD PANEL 283BS PER FEDEX DRWG SRZ-25-005 AGA3212
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD PANEL 242EF CORROSION ON INSERTS. FABRICATED NEW FLOOR BOARD PANEL 242EF PER SRZ-25-005 ADA8494
Part: NONE — NONE (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK FLOOR BOARD 282JF DAMAGED. FABRICATED NEW FLOOR BOARD PANEL 3282JF PER FEDEX DRWG SRZ-25-005
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK -CENTER FLOOR BOARD IN BETWEEN THE 76-106 RBL AND STA 1159-1219 MUTIPLE DAMGED AND CORRODED INSERT. FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005.
Part: FLOORBOARD — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO DECK CENTER FLOOR BOARD 283BS STA 5-93 TO 5-113 CORRODED AND MISSING IINSERT. FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CENTER FLOOR BOARD PANEL BETWEEN THE 76-106 RBL AND STA.1219-1256 MULTIPLE DAMAGED AND CORRODED INSERT. FABRICATED NEW FLOOR BOARD PANEL PER SRZ-25-005.
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK AFT FLOOR BOARD PANEL 283EF DELAM. FABRICATED NEW FLOOR BOARD PANEL# 283EF, AFA3163 PER FEDEX DRWG SRZ-25-005.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- CENTER FLOOR BOARD IN BETWEEN THE 76-106 RBL AND STA 1159 AND 6-70 HAS MULTIPLE DAMAGED AND CORRODED INSERTS. FABRICATED NEW FLOOR BOARD BETWEEN THE 76-106RBL AND STA 1159 AND 6-70 PER SRZ- 25-005.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- CENTER FLOOR BOARD IN BETWEEN THE 76-106RBL AND STA 1256-1301 HAS MUTLIPLE DAMAGED AND CORRODED INSERTS, FABRICATED NEW MAIN DECK FLOOR BOARD BETWEEN THE 76-106RBL AND 1256-1301 PER FEDEX DRWG SRZ-25-005
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK SEAT TRACK OUTB LOBE LOCATED AT STA 1841 AT LBL74 HAS EXFOLIATION CORROSION. NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE. SEE NON-ROUTINE N00068 WO# 81728 FOR DETAILS. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK SEAT TRACK INB LOBE LOCATED BETWEEN STA 1801 AND 1821 AT LBL74 HAS EXFOLIATION CORROSION. NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE. SEE NON-ROUTINE N00068 WO# 81728 FOR DETAILS. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK SEAT TRACK INB LOBE AT STA 1782 LBL 74 HAS EXFOLIATION CORROSION NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE. SEE NON-ROUTINE N00068 WO# 81728 FOR DETAILS. MAJOR REPAIR.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, EXFOLIATED CORROSION ON FLOOR SUPPORT AT CLIP NUT LOCATIONS STA 1361 RBL60. UPPER CARGO COMPT UNDER FLOOR AREA, STA 1361 RBL47-75, FLOOR SUPPORT AEA7326-6 REMOVED AND REPLACED IAW MD11 SRM 51-35-01-0G. SEE JPF.
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK STA 1761-1821 , 8,50L-27,50L FLOOR BOARD PANEL WEAR EXPOSING COMPOSITE MATERIAL. FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005 MAJOR REPAIR.
Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK STA 1821-1891,27.50L-47.50L FLOOR BOARD DELAMINATED, FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005 MAJOR REPAIR.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- CENTER FLOOR BOARD BETWEEN STA 1501 AND 5-93 HAS MULITIPLE DAMAGED AND CORRODED INSERTS. FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005 MAJOR REPAIR.
Part: SKIN — DAMAGED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX XORS 799, SLAT TRACK #14 CUT OUT HAS EXISTING REPAIR DOUBLER DOT. 54 0000356511 : LOGAN, DAVID D - 24-MAY-2022 17:58 EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-02 REPAIR 7, FIG. 201. REF. E.O. #1-5100-7-5001 ?MD-11 REPAIR CATALOG?, ATTACHMENT A-1 #22.
Part: BRACKET — CRACKED (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
AFT FUSELAGE,RIGHT HAND SIDW,FAIRING SUPPORT BRACKET, AJC7899-28 CRACKED. REMOVED AND REPLACED AJC7899-28 BRACKET REF SRM 51-31-01-OG AND DWG AJC7899
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CENTER FLOOR BOARD BETWEEN 10-27RBL AND STA 1401 AND 1501 HAS MULIPLE DAMAGED AND CORRODED INSERTS. FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005 MAJOR REPAIR.
Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 603 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: SPAR — NONE (ZONE 300) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H SIDE BANAGO #4 FITTING HAS REPAIR DOUBLER AT STA APROX YA 2164 DOT 46. EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 55-30-02-2R, REPAIR 5, FIG. 204.
Part: DOUBLER — UNKNOWN (LT WING) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 599 HAS EXISTING BEADED DOUBLER DOT 14. REMOVED EXISTING DOUBLER AND INSTALLED NEW REPAIR DOUBLER REF. MD-11 SRM 57-40-02-2R FIG. 203 REPAIR 15.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 785 LBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 35. REPAIRED PER SRM 53-00-52 FIG.201, REPAIR 1.
Part: SPAR — NONE (ZONE 300) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H SIDE BANAGO #4 FITTING HAS REPAIR DOUBLER DOT 45. EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 55-10-02-2R REPAIR 5, FIG. 204.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX 615 - 655, RBL 48 HAS EXISTING SEAT TRACK REPAIR DOT 29. SEATTRACK SPLICE REPAIR PER SRM 53-00-52 FIG. 201, REP. 1.
Part: NONE — NONE (NONE) · airframe 86,554 hrs · 16,394 cycles
CENTER CARGO COMP AT STA 1841, X= 45 HAS EXISTING ANGLE REPAIR ON CHANNEL EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED BY LCAG OPERATOR PER EI-53-0244.
Part: SKIN — NONE (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 372 HAS EXISTING RAP AROUND DOUBLER ON THE CUTOUT OF TELESCOPIC DUCT. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 10, FIG. 201, SHT. 1-5.
Part: STIFFENER — UNKNOWN (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: CENTER W/W, R/H SIDE STA APROX 1451 HAS EXISTING STIFFENER / DOUBLER REPAIR DOT 28. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED BY PREVIOUS OPERATOR LUFTHANSA EI: L2009A53B-002.
Part: SEAT TRACK — NONE (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 625 - 645 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 50. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM
Part: SKIN — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN CARGO DOOR AFT LWR CORNER STA APROX 755 - 785 HAS EXISTING REPAIR DOUBLER DOT 47. 0000356511 : LOGAN, DAVID D - 02-JUN-2022 15:23 EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 52-30-16, FIGURE 201, REPAIR 3. REF. E.O. #1-5100-7-5001 B6 PT1 ?MD-11 REPAIR CATALOG?, ATTACHMENT A-1 #47.
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1451 - 1531 RBL 75 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 645 HAS EXISTING BEADED DOUBLER . EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: DOUBLER — INOPERATIVE (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 1410 - 1530 LBL 47.5 HAS EXISTING SEAT TRACK REPAIR DOT 39. REPAIRED PER SRM 53-00-52 FIG.201. REPAIR 1.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX 585 - 645, RBL 27.5 HAS EXISTING SEAT TRACK REPAIR DOT 31. REPAIRED PER SRM 53-00-52 FIG. 201 REP. 1
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1391 - 1451 RBL 75 HAS EXISTING SEAT TRACK REPAIR DOT 43. REPAIRED PER SRM 53-00-52 FIG. 201, REPAIR 1.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 550 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT 1 - 4.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 524 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PERSRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX 625 - 645, LBL 48 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.
Part: NONE — NONE (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
L/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 183 HAS EXISTING ROUND REPAIR DOUBLER, DIM 3.5". EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-00-00 REPAIR GENERAL, FIG. 205.
Part: FLAP — DAMAGED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING O/B FLAP UPPER SKIN STA APROX. XOFH 764 - 773 HAS EXISTING BONDED REPAIR DOUBLER DIM. 9" X 5" DOT 22. 0000356511 : LOGAN, DAVID D - 21-JUN-2022 16:14 PREVIOUSLY INSTALLED REPAIR WAS DONE IN ACCORDANCE WITH SRM 57-50-80, REPAIR 1, FIGURE 201. 0000356511 : LOGAN, DAVID D - 21-JUN-2022 17:10 PREVIOUSLY INSTALLED REPAIR WAS DONE IN ACCORDANCE WITH SRM 57-50-80, REPAIR 1, FIGURE 201. REF. E.O. #1-5100-7-5001 ?MD-11 REPAIR CATALOG?, ATTACHMENT A-1 #22.
Part: FLAP — DAMAGED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 243 HAS EXISTING REPAIR DOUBLER DIM. 4" X 5" DOT 21. REPAIRED PER SRM 57-00-00 FIGURE 205, REF. FEDEX EA 1-5750-T0368054
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1361 - 1381 RBL 8.5 HAS EXISTING SEAT TRACK ATTACH LOBE REPAIR DOT 40. REPAIRED PER SRM 53-00-52 FIG. 201, REPAIR 1.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 625 - 645 LBL 8.5 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.
Part: DOUBLER — INOPERATIVE (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 511 HAS EXISTING BEADED DOUBLE. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPIAR 15, FIG. 203, SHT. 1-4.
Part: NONE — NONE (NONE) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING DLE TOP SKIN AT STA XDLE 309 - 329 HAS EXISTING REPAIR DOUBLER DOT 49. 0000356511 : LOGAN, DAVID D - 02-JUN-2022 15:30 EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-01, FIGURE 201, REPAIR 5. REF. E.O. #1-5100-7-5001 B6 PT1 ?MD-11 REPAIR CATALOG?, ATTACHMENT A-1 #49.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR RPEVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED P ER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 8055 LBL 27.5 HAS EXISTING SEAT TRACK REPAIR DOT 34. REPAIRED PER SRM 53-00-52 FIG. 201, REP. 1.
Part: SKIN — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 189 HAS EXISTING ROUND REPAIR DOUBLER DIM. 3.5". EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-00-00-2R FIG. 205.
Part: SKIN — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING SLAT #5 EXISTING FLUSH REPAIR STA APROX. XOS 661 - 668 ON THE OUTTER SKIN I/B TOP CORNER. EXISTING MEJOR REPAIR PREVIOSULY INSTALLED PER SRM 57-40-01-2R REPAIR 2, FIG. 201, SHT. 1 - 6.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 765 LBL 75.5 HAS EXISTING SEAT TRACK REPAIR DOT 33. REPAIRED PER SRM 53-00-52 FIG. 201. REP. 1
Part: SKIN — CRACKED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H FIXED WING LOWER SKIN ACCESS DOOR CUTOUT STA APROX XORS 683 - 714 HAS MULTIPLE BUSHING REPAIR DOT 22. REPAIRED PER SRM 57-20-02 FIG. 201 REPAIR 5
Part: SKIN — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING SLAT #4 HAS EXISTING FLUSH REPAIR STA APROX. XOS 652 - 660 ON THE OUTTER SKIN O/B TOP CORNER. (DIM 8" X 18") EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 57-40-01-2R REPAIR 2, FIG. 201, SHT. 1 - 6.
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1129 - 1269 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 38. REPAIRED PER SRM 53-00-02 FIG. 201, REPAIR 1.
Part: SKIN — CRACKED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H FIXED WING LOWER SKIN ACCESS DOOR CUTOUT STA APROX XORS 683 - 714 HAS MULTIPLE BUSHING REPAIR DOT 24. REPAIRED PER SRM 57-20-02 FIG. 201 REP. 5
Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 582 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57- 40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: FITTING — UNKNOWN (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H SIDE NOSE LANDING GEAR TRUNING STA APROX 595 HAS EXISTING STRAP REPAIR DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-10-14-2R REPAIR 2, FIG. 201, SHT. 1 -4. REPAIR REQUIRES REPETITIVE INSPECTION OF HFEC EVERY 250 CYCLES. HFEC INSPECTION WS CONDUCTED ON CURRENT "C-CHECK" CONDITIONS UNCHANGED.
Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 576 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 570 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: SKIN — NONE (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 372 HAS EXISTING RAP AROUND DOUBLER ON THE CUTOUT OF TELESCOPIC DUCT. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 10 FIG. 201, SHT. 1 - 5.
Part: NONE — NONE (NONE) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING DLE TOP SKIN AT STA XDLE 309 - 329 HAS EXISTING REPAIR DOUBLER DOT 48. 0000356511 : LOGAN, DAVID D - 02-JUN-2022 15:27 EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-01, FIGURE 201, REPAIR 5. REF. E.O. #1-5100-7-5001 B6 PT1 ?MD-11 REPAIR CATALOG?, ATTACHMENT A-1 #48.
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1129 - 1229 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 42. REPAIRED PER SRM 53-00-52 FIG. 201, REP.1
Part: FLAP — DAMAGED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 147 HAS EXISTING ROUND REPAIR DOUBLER DIM. 4" DOT 20. REPAIRED PER SRM 57-00-00 FIGURE 205. REF. FEDEX EA # 1-5750-T0368054 FOR COMPONENT TRACKING.
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 815 - 909 RBL 75.5 HAS EXISTING SEAT TRACK REPAIR DOT 37. REPAIRED PER SRM 53-00-52 F. 201, REP.1
Part: SEAT TRACK — NONE · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1229 - 1381 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.
Part: NONE — NONE (NONE) · airframe 86,554 hrs · 16,394 cycles
CENTER CARGO COMP AT STA 1841, X= 0 HAS EXISTING ANGLE REPAIR ON CHANNEL. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED BY LCAG OPERATOR PER EI-53-0244.
Part: FITTING — NONE (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H SIDE NOSE LANDING GEAR TRUNING STA APROX 595 HAS EXISTING STRAP REPAIR DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-10-14-2R REPAIR 2, FIG. 201, SHT 1 - 4. REPAIR REQUIERES REPETITIVE INSPECTION OF HFEC EVERY 250 CYCLES. HFEC INSPECTION WAS CONDUCTED ON CURRENT "C- CHECK" CONDITIONS UNCHANGED.
Part: SKIN — UNKNOWN (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: R/H WING SLAT #3 STA APROX XOS 456 HAS EXISTING REPAIR DOUBLER ON THE OUTTER LOWER SKIN. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 8, FIG. 201, SHT. 1 - 3 AND PREVIOUS OPERATOR LUFTHANSA TECHNIK ENGINEERING EI-57-0253.
Part: NONE — NONE (NONE) · airframe 86,554 hrs · 16,394 cycles
CENTER CARGO COMP AT STA 1841, X= -24 HAS EXISTING ANGLE REPAIR ON CHANNEL. EXISTING MAJOR REPAIR PREVIOSULY INSTALLLED BY LCAG OPERATOR PER EI-53-0244.
Part: SEAT TRACK — NONE (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 745 - 785 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.
Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 568 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.
Part: MEMBRANE — UNKNOWN (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
REPAIR ASSESSMENT: FWD AVIONICS COMP. FLITH DECK FLOOR LEVEL STA APROX. 366, X= 0, Z= -27 HAS EXISTING WEB REPAIR DOUBLER. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-10-51-2R REPAIR 1, FIG. 202, SHT. 1 - 4.
Part: NONE — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CENTER FLOOR BOARD BETWEEN STA 1381-1273 HAS MULITIPLE DAMGED AND CORRODED INSERTS. FABRICATED FLOOR PANEL REF FEDEX DRWG SRZ-25-005.
Part: NONE — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CENTER FLOOR BOARD IN BETWEEN 10-27 RBL AND STA 1501 AND 5-93 HAS MULIPLE DAMAGE AND CORRODED INSERTS. FABRICATED NEW FLOOR BOARD PER FEDEX DRWG SRZ-25-005.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO - STA 1368 LBL 50 - SEAT TREACK LOBE HAS CORROSION ON THOP & BOLLOM SIDE OF TRACK (MARKED) MAIN CARGO, STA 1368, LBL 50, SEAT TRACK ATTACH LOBE REPAIR PERFORMED IAW MD 11 SRM 53-00-52-2R REPAIR 5. *MAJOR REPAIR*
Part: DUCT — DELAMINATED (ZONE 400) · airframe 86,554 hrs · 16,394 cycles
#2 ENG INLET DUCT LH UPR EXT SKIN HAS DELAM AT PREVIOUS REPAIR. MRKD 30 IN FWD OF PNL 361EL REPAIRED PREVIOUSE REPAIR ON #2 ENG INLET DUCT EXTERNAL SKIN ON L/H SIDE 30 INCH FWD OF PANEL 361EL PER SRM 51-62-01-0G PAR.10.J PG.44.
Part: SKIN — CHAFED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
L/H WING FIXED L/E SKIN HAS SHALLOW WEAR FROM SLAT CONTACT BETWWEN SLAT TRACK #1 AND #3. MRKD REPAIRED L/H WING FIXED L/E SKIN FROM SLAT CONTACT BETWWEN SLAT TRACK #1 AND #3 PER MD11 SRM 57-40-02-2R FIG 201 REPIAR 4 SHEET 4.
Part: NONE — NONE (N/A) · airframe 86,554 hrs · 16,394 cycles
CENTER CARGO, STA 1801-1821, LONGERON 46R, AT SLPICE AREA, AFT OUTBOARD VERTICLE SIDE OF LONGERON HAS A CRACK. REPLACED CRACKED LONGERON 46R FROM STA 1811 TO 1828 AND FABRICATED NEW SPLICE REF SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND 202 SHEET 1, 2, AND 3 AND DWG AFA7098. "MAJOR REPAIR"
Part: SKIN — CORRODED (ZONE 300) · airframe 86,554 hrs · 16,394 cycles
R/H EMPENAGE FUSELAGE SKIN COMMON TO LOWER AFT FUSELAGE FAIRING NUTPLATE HOLES AT STA. 2140 TO 2160 HAS SURFACE CORROSION. MARKED RED. TRIMMED OUT CORRODED SKIN AND APPLIED DOUBLER REPAIR IAW SRM 53-70-01-2R REP3 FIG 201
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- SEAT TRACK AT STA 5-11 - 5-52 AND THE 10 LBL HAS 2 LOCATIONS WITH PITTING CORROSION. REPAIRED SEAT TRACK BETWEEN STA 1371-1510, LBL8 AT EXISTING SPLICES LOCATIONS REF SRM 53-00-52-2R FIG 201 REPAIR 1 SHEET 1. ALONG WITH JPF ITEMS 1-7.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- SEAT TRACK AT STA 1501 - 5-11 AND THE 10LBL HAS 4 LOCATIONS WITH EXFOLIATING CORROSION. REPLACED DAMAGED SEAT TRACK, FROM STATION 1510 - (5-113), LBL8 REF. SRM 51-31-01 VOL. 2, SR10-53-002 DWG, SRM 53-00-52-2R FIG 201 REPAIR 1 SHEET 1.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - FLOOR SUPPORT SHOWS SURFACE CORROSION AT STATION 1821 FROM RBL 52 TO RBL 66 REMOVED AND REPLACED FLOOR SUPPORT P/N AGA3814-4 AT STA 1821 FROM RBL 52 TO RBL 66 REF SRM 51-31-01-OG AND DWG AGA7510
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- FLOOR SUPPORT SHOWS SURFACE CORROSION AT STATION 1821 FROM RBL 70 TO RBL 106 REMOVED AND REPLACED FLOOR SUPPORT P/N AGA3814-34 AT STA 1821 FROM RBL 70 TO RBL 106 REF SRM 51-31-01-OG AND DWG AGA7510
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER FUSELAGE MD SEAT TRACKS AT STA1661-1791/LBL74 SUSPECT SURFACE CORROSION AT MULTIPLE HOLES (MARKED). REMOVED CORROSION FROM UPPER FUSELAGE MD SEAT TRACKS AT STA1661-1791/LBL74 PER MD-11 SRM 51-21-01-0G AND REPAIRED INB LOBE BTWN STA 1741 AND 1761 PER MD11 SRM 53- 00-52-2R FIG 201 REPAIR 4 SHEET 2. "MAJOR REPAIR"
Part: STIFFENER — CRACKED (ZONE 300) · airframe 86,554 hrs · 16,394 cycles
NO.2 ENGINE PYLON, CRACK ON WEB SUPPORT ANGLE AT FWD END OF LOWER BOAT TAIL SEGMENT. (MARKED #5) REF JPF ITEMS 1 TO 11, REMOVED AND REPLACED BROKEN 1378M76P161A STIFFENER, REF SRM 54-51-71-01, AND GMM 07-0-1001 SEC. 7 (A) 2.C
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK HAS CORROSION AT STATION 1791 RBL 50 SEAT-TRACK ATTACH LOBE REPAIR PER SRM#53-00-52-2R FIG-201 SHT-1 PG-26
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- SEAT TRACK BETWEEN STA 5-32 - 5-73 AND THE 76 RBL HAS 4 4 LOCATIONS WITH PITTING CORROSION. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION AT MAIN DECK BETWEEN STA 5- 00 AND 5-123 AT 76 RBL REFERENCE SRM 53-00-52-2R AND FEDEX DRAWING SR10-53-002. "MAJOR REPAIR".
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- SEAT TRACK IN BETWEEN STA 1481 - 5-32 AND THE 106 RBL HAS 2 LOCATIONS WITH PITTING CORROSION. REPLACED DAMAGED SEAT TRACK, FROM STATION 1510 - (5-123), LBL106 WITH NEW AND SPLICES AT STA 1510 AND 5-123, RBL 106 REF. SRM 51-31-01-OG, SR10-53-002 DWG, SRM 53-00-52-2R FIG 201 REPAIR 1 SHEET 1 AND JPFS.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK LOBES/NUTPLATE HOLES HAVE SURFACE CORROSION AT STA 760, LBL 47. ENTERED IN ERROR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK LOBES/NUTPLATE HOLES HAVE SURFACE CORROSION AT STA 760, LBL 47. REMOVED AND REPLACED FLOOR SUPPORT AGA7085-501 AT STA 1911 AND LBL 59-RBL 59 REF MD11 SRM 51-31-01-0G AND MD11 DRWG AGA7085 & ASSY DRWG AGA7127. MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- FLOR SUPPORT BRACKET AT STA 1501 BETWEEN THE 10-27 LBL HAS 2 LOCATIONS WITH EXFOLIATING CORROSION. REMOVED AND INSTALLED NEW/FABRICATED SUPPORT BRACKETON MAIN DECK AT STA 1501 BETWEEN THE 10-27 LBL REF, MD-11 SRM 51-31-01-0G AND DGW NO. AEA7330 "MAJOR REPAIR"
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK SHOWS SURFACE CORROSION FROM STATION 1715 TO 1734 AT RBL 102 REPARED CORRODED SECTION OF SEAT TRACK PER MD 11 SRM 53-00-52-2R FIG 201. SEE JPF FOR REPAIR DETAILS . MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO FROM STA 5-93 TO STA 1561 AT RBL 76 SEAT TRACK CORRODED. REPLACED CORRODED SEAT TRACK FROM STA 1531 TO 1571, RBL 75.25 IAW MD11 SRM 53-00- 52-2R FIG. 201 SHEET 1-3.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO STA 1561 TO 1661 AT RBL 107 SEAT TRACK CORRODED AROUND CLIP NUT HOLES. 0004079295 : VUKI, ESAFE - 18-APR-2022 20:16 INSTALLED SEAT TRACK AND SPLICE ON MAIN CARGO AT STA 1561 TO 1661 RBL 107 PER SRM 53-00-52-2R. SEALED PER SRM 51-41-01-OG. INSTALLED HI-LOCKS PER FDX DRAWING SR10-53- 002, AND SRM 51-31-01-OG
Part: FLOOR SUPPORT — CORRODED (200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- FLOOR SUPPORT BRAKET AT STA1501 CENTER BL HAS EXFOLIATING CORROSION. REMOVED AND INSTALLED NEW/FABRICATED SUPPORT BRACKETON MAIN DECK AT STA 1501 BETWEEN THE BL 0 REF, MD-11 SRM 51-31-01-0G AND DGW NO. AEA7330. "MAJOR REPAIR"
Part: FLOOR SUPPORT — CORRODED (MAIN DECK) · airframe 86,554 hrs · 16,394 cycles
MD AFT CTR BUTTLINE/STA 1761 FLOOR SUPPORT BRACKET HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FLOOR SUPPORT ACA3140-505 REF DWG ACA3140 AND MD11 SRM 51-31-01-0G "MAJOR REPAIR"
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK, STA 1119, LBL 27, SUSPECT CORROSION ON SEAT TRACK. REPLACED DAMAGED SECTION OF THE SEAT TRACK AT STA 1109-1129 LBL 27 REF MD11 SRM 53-00-52-2R REPAIR 1, FIG. 201, SHEET 1-3 AND FEDEX DRW. SR10-53-010. MAJOR REPAIR.
Part: SKIN — GOUGED (ZONE 100) · airframe 86,554 hrs · 16,394 cycles
OUTER SKIN, LOWER FUSELAGE, AFT OF CENTER MAIN GEAR, APPROX STA. 5-93 TO 5-73, BETWEEN LONGERON R49-R50, SKIN HAS A NICK AND DENT. PERFORMED MAJOR REPAIR PER SRM 53-00-01, REPAIR 1,FIG 201 SHEETS 9-10. SRM 51-33-01- 0G.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK, STA 859-899, RBL 7, SUSPECT CORROSION ON SEAT TRACK HAT WHERE FLOORBOARD SITS. REMOVED AND REPLACED SEAT TRACK SECTION AND INSTALLED SPLICES IAW SRM 53-00-52-2R, DWG# NDA6792, & SR10-53-010-22
Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK CORRODED AT RBL 47,STA 1561 TO 1661. REMOVED AND REPLACED SEAT TRACK AT STA 5-113-1641 RBL 47 REF MD-11 SRM 53-00-52-2R AND SRM 51-31-01-OG. "MAJOR REPAIR"
Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
SUPPORT BRACKET P/N:AGA3122-22 AT STA 1931 R/H L-9 IS CRACKED. REMOVED, FABRICATED AND INSTALLED AND INSTALLED CLIP P/N AGA3122-22 REF, MD-11 SRM 51-31-01-21-0G AND DOUGLAS DWG AGA3122 MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK SEAT TRACK APPROX STA 1877 LBL 47. SEAT TRACK LOBE CORRODED. REPLACED CORRODED SECTION OF THE SEAT TRACK AT STA 1862-1887 LBL47 REF MD11 SRM 53-00-52-2R REPAIR 1, FIG. 201 , SHEET 1-3 AND FEDEX DWG SR10-53-002. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK AT STA 1841 LBL 67 HAS EXFOLIATION CORROSION BEYOMD LIMITS. INSTALLED NEW SEAT TRACK SECTION PN:AFA7789-543 FROM STA 1771 TO 1887 LBL 75.25/LBL 67 WITH NEW SPLICE P/N: SR10-53-010-21 REF, MD-11 SRM 53-00-52-2R REPAIR 1 FIG 201, AND FEDEX DGW NO. SR10-53-002 REV A. MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO FLOOR BOARD SUPPORT AT STA 1891 LBL 72 HAS EXFOLIATION CORROSION BEYOND LIMITS. REMOVE AND REPLACE FLOOR SUPPORT P/N: AGA3814-7 AT ST 1891 LBL 72. REF MD-11 SRM 51-31-01-OG, AND DOUGLAS DRWG AGA3814. "MAJOR REPAIR"
Part: SUPPORT — CRACKED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK AT STA 1885 LBL 26 HAS EXFOLIATION CORROSION BEYOND LIMITS. REPLACED SEAT TRACK AT STA. 1885 LBL 26 REF. DRWG. AGA7544, SRM 51-31-01-OG, SRM-33-01-OG, AND JPF ITEMS -MAJOR REPAIR-
Part: TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK AT STA 1901 LBL 23 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED NEW SECTION OF SEAT TRACK AT STA. 1901 LBL 23 REF SRM 53-00- 52-2R REPAIR 1, FIG. 201, SHEET 1-3 AND REF DOUGLAS DRWG AFA7795. "MAJOR REPAIR"
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK AT STA 1986 TO 2000 LBL 56 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED MAIN CARGO SEAT TRACK SUPPORT AFT OUTBOARD STA. 1986 TO 2000 LBL 56 IAW DAC DWG AGA7551-507 AND SRM 51-31-01-0G.
Part: SUPPORT — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO SEAT TRACK AT STA 1901 TO 2006 RBL 26 HAS SURFACE CORROSION. REMOVED AND REPLACED SEAT TRACK STA1901 TO 2006 RBL 26 REF DWG 7087 AND SRM51-31- 01-OG & SRM51-33-01-OG.
Part: SPAR CAP — CRACKED (ZONE 300) · airframe 86,554 hrs · 16,394 cycles
L/H HORIZONTAL STAB FRONT UPPER SPAR AT STA. XE 51.00 IS CRACKED AT TOP FLANGE. MARKED. REPAIRED PER EA# 1-5510-T0367033 - STABILIZERS - HORIZONTAL STABILIZER - LH HORIZONTAL STABILIZER FRONT SPAR UPPER CAP XE 51.00 - CRACK REPAIR
Part: SUPPORT — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO FLOOR SUPPORT AT STA 1911 RBL 36 HAS SURFACE CORROSION. REMOVED AND REPLACED FLOOR SUPPORT AGA7085-501 AT STA 1911 AND LBL 59-RBL 59 REF MD11 SRM 51-31-01-0G AND MD11 DRWG AGA7085 & ASSY DRWG AGA7127. SEE JPF MAJOR REPAIR.
Part: TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK- SEAT TRACK CORRODED AT STATION 1851 RBL 64. REMOVED AND REPLACED DAMAGE SECTION OF SEAT TRACK WITH FABRICATED SEAT TRACK AND SPLICE REF MD11 SRM 53-00-52-2R REPAIR 1 FIG. 201 SHEET 1-3. "MAJOR REPAIR"
Part: NONE — NONE (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON FLOORBOARD SUPPORT AT CLIP NUT LOCATIONS STA 1321 BL 0. (MARKED #25) REMOVED AND REPLACED FLOORBOARD SUPPORT BRACKETLOCATED AT MAIN CABIN STA 1321 BTWN STR9L AND STR9R PER DWG AEA0392 AND SRM 51-31-01-0G. 'MAJOR REPAIR'
Part: SUPPORT BRACKET — GOUGED (NR 1 PYLON) · airframe 86,554 hrs · 16,394 cycles
NO.1 ENG PYLON, PYLON BRACKET LAND FOR PNLS 437EL AND 437AR HAS NUMEROUS AREAS OF DEEP GOUGES/GALLING ON TOP ARCH OF BRACKET. REMOVED WORN SUPPORT BRACKET AND REPLACED WITH FABRICATED BRACKET IAW DAC DWG AUB7564 AND REF SRM 51-31-01-0G.
Part: SUPPORT — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK CORRODED FROM STATION 1953 TO STATION 1981 RBL 60 REMOVED AND REPLACED SEAT TRACK SUPPORT STA 1953 TO 1981 RBL 60 REF DWG AGA7544 AND AGA7551, SRM 51-31-01-0G/SRM 51-35-01-0G/SRM 51-33-01-0G. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON SEAT TRACK AT CLIP NUT LOCATIONS STA 1280 - 1321 RBL 8. (MARKED #27) PERFORMED STANDARD SEAT REPAIR PER SRM#53-00-52-2R.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK - SEAT TRACK CORRODED FROM STATION 1953 TO STATION 2000 RBL 68. INSTALLED NEW SEAT TRACK SECTION FROM STA1878 TO STA2007 RBL 107.25 WITH NEW SPLICE REF, EA#:1-5310-T0368319. "MAJOR REPAIR".
Part: NONE — NONE (N/A) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON FLOORBOARD SUPPORT AT CLIP NUT LOCATIONS STA 1219 RBL 95. (MARKED #3) REMOVED AND REPLACED AEA0395-501 REF AEA0395
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, EXFOLIATED CORROSION ON FLOORBOARD SUPPORT STA 1159 LBL 55. (MARKED #10) REPLACED SUPPORT PER DAC DWG# AEA7326
Part: FRAME — BENT (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK STA. 695 BETWEEN L13R & L14R FOUND IMPACT DENT ON FRAME (MARKED) REPAIRED DAMAGED FRAME AT STA. 695 R/H BETWEEN LONGERON 13 AND 14 REF. MD-11 SRM 53-00-07-2R FIG. 201. REPAIR 4. *MAJOR REPAIR* .
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON FLOORBOARD SUPPORT AT CLIP NUT LOCATIONS STA 1256 RBL 95. (MARKED #4) REMOVED AND REPLACED AEA0395-501
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO COMPT, STA 1889 72RBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED AND REPLACE FLOOR SUPPORT REF. DWG. AGA3814.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO COMPT, STA 1321 20RBL FLOOR SUPPORT HAS CORROSION . REMOVED DAMAGED FLOOR SUPPORT FROM STA. 1321 RBL20, FABRICATED NEW SUPPORT FROM P/N S2929169T ALODINED AND PRIMERED NEW SUPPORT AND INSTALLED ON A/C AT STA 1321 RBL20 REF. MD-11 SRM 51-31-01-0G, 51-21-01-0G, & DAC. "MAJOR REPAIR"
Part: NONE — NONE (N/A) · airframe 86,554 hrs · 16,394 cycles
UPPER CARGO COMPT UNDER FLOOR AREA, LIGHT CORROSION ON FLOORBOARD SUPPORT AT CLIP NUT LOCATIONS STA 1219 RBL 95. (MARKED #3) REMOVED AND REPLACED AEA0395-501 REF AEA0395
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN DECK CARGO COMPT,STA1321 TO 1380 8RBL SEAT TRACK HAS CORROSION, CHECK TOP AND BOTTOM SIDE. REMOVED AND REPLACED SEAT TRACK AT STA 1321 TO 1380 REF MD-11 SRM 51-31-01-0G, SR 10-53-002 DWG, SRM 51-41-01-0G AND SRM 53-00-52-2R. MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK COMPT, STA 1481 94RBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED AND REPLACED PER DWG AEA 7330 AND SRM 51-31-01
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK, STA1389 50LBL SEAT TRACK HAS CORROSION ON TOP AND BOTTOM SIDES (MARKED) BLENDED/ REMOVED CORROSION ON MAIN CARGO DECK AT STA. 1389 50LBL. REPAIR FOUND TO BE WITHIN LIMITS REF. MD-11 SRM 53-00-52-1A MAJOR REPAIR
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK COMPT, STA 1381 10RBL FLOOR SUPPORT CORROSION (MARKED) REMOVED AND REPLACED FLOOR SUPPORT IAW MD-11 SRM 53-40-51-01 FIG. 1 SHT. 2 REF. DOUGLAS DWG AEA7330.
Part: SUPPORT — CRACKED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK, STA1481 54LBL FLOOR SUPPORT DAMAGE (MARKED) 0004002945 : FICKES, KYLE S - 20-MAR-2022 13:16 REMOVED DAMAGED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT, PROCESSED AND INSTALLED REF. DAC. DWG. AEA7326 & MD-11 SRM 51-31-01-0G. "MAJOR REPAIR"
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK COMPT, STA 1381 108RBL SEAT TRACK CORROSION (MARKED) REPLACED DAMAGED SEAT TRACK, FROM STA 1381-1451 RBL 106 WITH NEW SPLICES AT STA 1381 AND 1451, RBL 106, REF. SRM 51-31-01-0G, DWG SR10-53-002, SRM 53-00-52-2R FIG 210, REPAIR 2 AND JPFS.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK, STA 1481 82LBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED DAMAGED FLOOR SUPPORT AND FABRICATED AND INSTALLED NEW FLOOR SUPPORT PER, DWG. AEA7330 AND AEA0364
Part: SEAT TRACK — CORRODED (N/A) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK, STA 1469 73LBL SEAT TRACK HAS CORROSION TOP AND BOTTOM SIDE (MARKED) REPLACED SEAT TRACK FROM STA. 1139 TO 1531 IAW MD11 SRM 53-00-52-2R FIG.201. SHEET 1- 3 REPAIR 1.
Part: SPAR — CORRODED (ZONE 500) · airframe 86,554 hrs · 16,394 cycles
L/H WING REAR, SPAR UPPER CAP ANGLE, REAR FLANGE AT WING STA 670 XORS, UPPER SURFACE HAS CORROSION APPROX THREE INCHES IN LENGHT. (MKD) REPAIRED PER EA # 1-5710-T0367013 WING - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP STA. XORS 675 - 680.5 AND XORS 785 - 798 - REWORK.
Part: DOUBLER — NONE · airframe 86,554 hrs · 16,394 cycles
FWD. CABIN AREA: ADDITIONAL OPENING IS REQUIRED TO FACILIATE STRUCTURAL SAMPLING INSPECTION FROM STA. 394-555 LONGERONS 27L-27R, AS PER WC 53S1808 SEQ. 896 STEPS 3A. (1),(3),(5),(7). REMOVED EXISTING DOUBLER AND INSTALLED NEW REPAIR DOUBLER REF. MD-11 SRM 57-40-02- 2R FIG. 203 REPAIR 15.
Part: PANEL — CORRODED (NR 1 NACELLE) · airframe 86,554 hrs · 16,394 cycles
NO.1 ENG PYLON, PANEL LAND FOR 437CL AND 437AR HAS EXCESSIVE GALLING,PITTING CORROSION ON TOP ARCH AREA OF BRACKET. REMOVED WORN SUPPORT BRACKET AND REPLACED WITH FABRICATED BRACKET PER REF DAC DWG AUB7564 AND SRM 51-31-01-0G.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 86,554 hrs · 16,394 cycles
MAIN CARGO DECK FLOOR PANEL AT STA 1481 LBL 80, PANEL INSERTS AND SCREWS ARE CORRODED. (MKD) FABRICATED FLOOR BOARD AEA 7542-9 (271JF) REF DWG SRZ-25-005.
Part: SKIN — CRACKED (ZONE 600) · airframe 86,554 hrs · 16,394 cycles
R/H WING BOTTOM FIXED L/E, FUELING PANEL CUTOUT I/B CORNER CRACKED (MARKED) PERFORMED MAJOR REPAIR PER SRM 57-40-01-2R REPAIR 18.
Part: BEAM — CRACKED (R4 DOOR) · airframe 86,554 hrs · 16,394 cycles
R4 DOOR - BEAM 2 CRACKED AT FWD STOP. REMOVED AND REPLACED BEAM PER EA.1-5210-T-0367036