N554FE
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORP | Operator | 2008-06-14 – 2008-06-14 | Operator named in NTSB report |
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | 2008-06-14 – 2008-06-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
MANUAL DOOR LIFT BAR ON R1 DOOR DISCONNECTED. REINSTALLED LIFT BAR IAW MM 52-10-01-50, AND 25-61-02-5.
FOUND 15" LONG CRACK IN THE CAC AFT WALL LT SIDE ABOVE THE NR 2 PNUEMATIC DUCT FEED THROUGH DURING FUSELAGE PRESSURIZATION CHECK. RECEIVED FINAL EA 8-5300-T0326238; FUSELAGE, GENERAL-STA 1159 PRESSURE BULKHEAD REPAIR, LT SIDE, COMPLIED WITH.
DURING CLIMB GOT LEVEL 2 ENG 3 LOOP A. COMPLIED WITH CHECKLIST B LOOP TESTED GOOD. MEL 02 JUN16 04:05. RELEASED FOR SERVICE IAW MEL 26-11-01-01 CATEGORY C EXPIRATION 11JUN16. ENG NR 3 LOOP A INOPERATIVE, USE LOOP B. PLEASE TROUBLESHOOT ID & UPDATE ITEM WITH REQUIRED PART NUMBERS. R & R CDP BLEED AIR MANIFOLD ASSY REF ESM 72-00-00, STEP-S, PRE SB 75-041. RAN ENGINE. LEAK CK GOOD. OK FOR SERVICE.
MULTIPLE FAN BLADES DAMAGED ON NR 3 ENG DUE TO BIRD STRIKE. DURING BORESCOPE OF NR 3 ENG FOR BIRD STRIKE, FOUND LARGE TEAR ON LE 10TH STAGE THROUGH PORT B1-10. REPLACED NR 3 ENG.
TWO CRACKS EXIST IN LT NR 1 LE SLAT. ONE IS 1.4 INCHES LONG, THE OTHER, 0.8 INCHES LONG. REPAIRED LT NR 1 SLAT SKIN LE IAW SRM 57-10-00. RCS TRACKING ON EA 8-5710-T0319366. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
R1 DOOR SLIDE LIGHT DOES NOT TEST. R & R BATTERIES FOR PRESS TEST LIGHT IAW AMM 25-61-02-2. OPERATIONS CHECKED NORMAL, OK TO CONTINUE.
FORWARD LOWER CARGO FIRE WARNING, AGENT DISCHARGED. NO SMOKE OR FIRE WAS FOUND, FALSE INDICATION. REMOVED FREIGHT & PLACED ALL LOWER CARGO COMPARTMENTS ON MEL. DISCONNECTED ALL 8 LOWER CARGO SMOKE DETECTORS IAW EA 8-2617-T0318588 & PLACED THE NR 1 & 2 FIRE EXTINGUISHER BOTTLES ON MEL WITH ALL LOWER CARGO COMPARTMENTS VOID.
IN CRUISE WITH WING ANTI-ICE ON WE RECEIVED NR 3 MANIFOLD FAIL LIGHT IN SWITCH & RECEIVED MANIFOLD FAIL INDICATION ON SYNOPTIC, NO MANIFOLD FAIL NR 3 ALERT WARNING THOUGH. R & R RT WING PRESSURE SWITCH IAW AMM 36-23-03-4. OPERATIONS CHECKED NORMAL, OK TO CONTINUE.
RIGHT LOWER HORIZONTAL STAB FAIRING IS DELAMINATED, SECTION ADJACENT TO ATTACH POINT. REPAIRED RT HORIZONTAL STAB LOWER FAIRING IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.
RIGHT WING, LOWER WING ATTACH PANEL SURFACE 618 GB AFT OF SLAT TRACK NR 8 HAS A 1 INCH CRACK. DOT 1 REPAIR COMPLIED WITH IAW SRM 57-10 00 FIG 49 SHEET 1 THROUGH 4 VOL 1.
MAIN DECK STATION 1551 LT 27.50 SEAT TRACK DAMAGED. R & R DAMAGE SEAT TRACK AT STATION 1551 LT 27.50 IAW SRM 53-70-00 VOL I.
MAIN DECK STATION 1310 RBL 27.50 SEAT TRACK DAMAGED. REMOVED DAMAGED SEAT TRACK AT MAIN DECK STATION 1259 - 1330 RBL 27.50 IAW SRM 53-70-00 FIG 1A VOL I EEL 537397 11/23/14. REPLACED DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 1A VOL I.
CAC STATION 1156 LT OTBD FRAME AT FLOOR LINE, FRAME FLOORBEAM FITTING CRACKED. REPAIRED FRAME FLOORBEAM FITTING IAW SRM 53-30-00 FIG 7.
LEFT WING PANEL ARC0446-501 IS DELAMINATED & CORRODED. CUT OUT DAMAGED AREA. REPAIR PANEL ARC0446-501 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 71-21-02 VOL II.
RIGHT WING PANEL ARC0446-502 IS SEPARATING ON CORNERS. REPAIR PANEL ARC0446-502 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
VERTICAL STAB LT SIDE ACCESS PANEL 374EL HAS DELAMINATION. REPAIR DELAMINATION ON PANEL 374EL IAW SRM 51-71-00 VOL II.
RIGHT INBD ELEVATOR TOP SURFACE HAS MULTIPLE DENTS, APPROX 40 INCHES OTBD OF DETACHABLE ELEVATOR. RIGHT INBD ELEVATOR TOP SURFACE HAS 5 DENTS WITHIN LIMITS & 1 OUT OF LIMITS AT STATION XE 142. REMOVED DAMAGE & INSTALLED DOUBLER AT STATION XE 142 IAW SRM 55-00-01 FIG 3 SHT 2.
RIGHT WING OTBD FLAP HAD SKIN AT INBD HINGE AREA LOWER SECTION WAVY & CREASED, MARKED DOT 7. REPAIRED FLAP SKIN IAW SRM 57-10-00 FIG 85 SHEET 2.
RIGHT WING OTBD LAP INBD HINGE PANEL 635AR, PN ARC0794-506, MISSING TOP SKIN 4 INCH X 6 INCH SECTION. REPAIRED MISSING TOP SKIN ON PANEL 635AR IAW SRM 51-71-00 VOL II.
MAIN DECK STATION 1310 RBL 27.50 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.
CAC STATION 1156 LT OTBD AT FLOOR LINE, FRAME & FLOORBEAM FITTING CRACKED. FITTING REMOVED AND REPLACED REFERENCE SRM 53-30-00 FIGURE 7 VOLUME 1.
CENTER WW LT FWD CORNER BULKHEAD DOUBLER HAS A CRACK IN THE RADIUS ON THE LOWER END OF THE BRACKET AT BS 1381. REMOVED DAMAGED DOUBLER AND INSTALLED NEW SERVCEABLE DOUBLER IAW DRAWING NEA6078 AND SRM 51-33-01 VOL 2.
LEFT WING NR 12 SLAT TRACK CUT OUT HAS EVIDENCE OF CRACK. LT WING NR 12 SLAT CUT OUT NEEDS NDT VERIFICATION. VERIFIED & MARKED THE END OF THE CRACK WITH HFEC IAW NDT SPM PART 6, 06-00-06. REMOVED FASTENERS FROM NR 12 SLAT TRACK CUT OUT AREA, TO FACILITATE INSTALLATION OF DOUBLER IAW 51-31-01. REMOVE DAMAGED AREA & CRACK IAW SRM 57-10-00 VOL 1 FIG 68 SHEET 1. NDT REQUESTED TO VERIFY ALL DAMAGE REMOVED. PERFORMED HFEC INSP IAW NDT SPM PT 6 OF CUT OUT AREA, ALL OF THE CRACK HAS BEEN REMOVED. FABRICATED DOUBLER & FILLER IAW SRM 57-10-00 FIG 68. MATERIAL VERIFIED & OK TO INSTALL. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. STILL REQUIRES EDGE SEALANT & PAINT.
NUMBER 7 SLAT CUT OUT HAS CRACK INDICATION HAD A 1 INCH BLACK SMOKE LINE. WIPED AWAY, STILL HAS A SLIGHT APPEARANCE OF A CRACK. REMOVED DAMAGED SKIN USING .5" RADIUS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. PERFORMED HFEC OF THE CUT OUT AREA IAW NDT SPM PART 6, 06-00-06, NO CRACKS NOTED. FABRICATED, DRILLED & TRIMMED EXTERNAL DOUBLER & FILLER IAW SRM 57-10-00 VOLUME 1 FIGURE 68. DOUBLER MADE FROM 6AL-4V .063" TITANIUM MP0642228, FILLER FOR SKIN CUT OUT MADE FROM .090" 7075-T6 ALUMINUM MP1681501. INSTALLED DOUBLER IAW SRM 57-10-00 FIG 68.
LEFT HORIZONTAL STAB UPPER SPAR CAP HAS A APPROX 1.50" CRACK EMANATING FROM FROM A PREVIOUS REPAIR AT XFS 88.834. REPAIRED IAW SRM 55-20-00 FIG 8.
DOOR SLIDE TEST BUTTON WILL NOT TEST. REPLACED BATTERIES AND BULBS REF AMM 25-61-01-2-0, OPS CHECKED OK.
DURING POST FLIGHT FOUND EMERGENCY LIGHT TEST FAILED, WITH EMERGENCY BATTERY 1 LOW ALERT DISPLAYED. R & R EMERGENCY LIGHTS POWER SUPPLY, AS REQUIRED OPS CHECKED GOOD. REF MM 33-51-01-4-0.
ON DECENT, NR 3 ENGINE BECAME UNCONTROLLABLE, A/T OFF OR A/T ON, ENGINE SURGE +/- 20 PERCENT ALL INDICATION. ENGINE SHUTDOWN PERFORMED AND WINDMILLED APPROX 20 MINUTES. R & R NR 3 ENGINE CIT SENSOR, REF AMM 73-20-02-2. INSTALLED NR 3 ENGINE MEC AND FUEL PUMP REF AMM 73-20-01-2 AND 73-12-02-2. VSV RIG CHECKED GOOD. PERFORMED IDLE RUN AND LEAK CHECK IAW JRH. NO LEAKS NOTED. PERFORMED GROUND IDLE, FLIGHT IDLE AND MAX POWER ASSURANCE IAW JRH CHAPTERS 4, 5 AND 7. ALL CHECKS WITHIN PARAMETERS. OK FOR SERVICE.
L1 DOOR DISARMED LIGHT INOP. RELAMPED AS REQUIRED IAW MM 33-00-00-2-0. OPS CHECK GOOD.
R1 DOOR SLIDE LOW PRESS LIGHT INOP. REPLACED BATTERIES IAW AMM 25-61-03-2-0 AND TESTED IAW AMM 25-61-03-5-0, CKS OK.
LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RAN QRH AND STILL UNABLE TO BRING GEAR LEVER TO UP POSITION. BURNED OFF EXCESS FUEL AND LANDED WITHOUT INCIDENT. UNABLE TO MOVE GEAR HANDLE OUT OF DOWN DETENT WITH OR WITHOUT OVERIDE BUTTON. FOUND TRIM CYLINDER INTERLOCK FUSE TRIPPED, RESET SAME IAW AMM 32-31-06-2. NOW ABLE TO MOVE GEAR HANDLE TO UP POSITION WHILE PUSHING OVER RIDE. BLED LT MAIN GEAR TRIM CYLNDER RELIEF VALVE IAW AMM 32-37-03-2. GEAR HANDLE INTERLOCK OPS NRML REF 32-37-03-2. ACFT OK FOR SVC.
ENG 2 EGT HI" LEVEL ONE ALERT DURING DESCENT. EGT WAS 1092 IN RED.MOVED THROTTLE TO IDLE, APPROX 20 SECONDS LATER ALERT CHANGED TO LEVEL 1 "ENG 2 EXCEEDAMCE", TEMP INDICATION DECREASED TO AROUND 900. APPROX 10 SECONDS LATER TEMP INCREASED ABOVE RED LINE WITTH LEVEL 2 ALERT AGAIN. ENGINE SHUT DOWN IAW CHECKLIST. REMOVED NR 2 ENGINE EGT LEADS AND EGT HARNESSES AND BEGAN INSTALLATION. REF. MD10 AMM 77-21-01-2, 77-21-02-2. REQUIRES OPS CK. PERFORMED NR 2 ENG HIGH POWER RUN. EGT PARAMETERS REMAINED NORMAL, NO FLUCTUATIONS OR DEFECTS NOTED. REMOVED AND REPLACED NR 1 AND NR 3 AIU'S.
AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED FIRE CREW FOUND NO FIRE EVIDENCE ON A/C. REMOVED AND REPLACED 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT.
AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED. FIRE CREW FOUND NO FIRE EVIDENCE ON A/C. R&R 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT
ON MX POST FLIGHT INSP FOUND RT OUTBOARD ELEVATOR DAMAGED. APPEARS TO BE LIGHTNING STRIKE AT OUTBOARD TIP AND TIP TRAILING EDGE OF ELEVATOR ACCOMPLISHED RT OUTBOARD ELEVATOR INSTALLATION STEP NR 3-B ITEM NR 18 AND STEP NR 3-C 1 THRU 9.
LT KEEL BEAM WEB AT STA 1501 Z= -40 APPROX FOUND CRACK ON EXISTING REPAIR. REPAIR WEB IAW SRM 53-00-01 FIG 10 VOL 1.
MAIN CABIN CTR WING SECTION UPPER SKIN CORROSION UNDER HEAD OF FASTENERS. REPAIRED IAW FEDEX EA 8-5730-103734.
LT WING INB'D FLAP DENTS ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 4 VOL.1.
EXTERNAL FUSELAGE STA 475 RT LOWER FUSELAGE CUT OUT NOSE W/W. REPAIRED IAW FEDEX EA8-5310-105639.
LT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIR IAW SRM 57-10-00 FIGURE 68 VOL 1 SHT 1-3.
RT MLG W/W FOUND CORROSION ON PRESSURE PANEL STA 1381 UNDER SLANT PANEL. REPAIRED IAW FEDEX EA 8-5730-103734.
LT WING LOWER SURFACE NR 40 HEAD FASTENERS ON SKIN FOUND MODERATE CORROSION. REPAIRED IAW FEDEX EA 8-5730-103735.
HORIZONTAL STAB SPAR CAP FOUND CRACK LONG .750" AND .800" REPAIRED IAW FEDEX EA 8-5510-96110.
RT WING L/E AT SLAT TRACK HOLE NR 2 FOUND SKIN CORRODED. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1.
LOWER EXT FUSELAGE FOUND DENT 1.5" BY 1" DEPTH 0.050". REPAIRED PER NRC IC02006.
LWR FUSELAGE EXT SKIN FOUND DEEP DENT 2" BY 2" DEEP 0.07". REPAIRED IAW FEDEX EA 8-5310-96119.
RT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 VOL.1 SHT 1-3.
LOWER FWD CARGO DOOR DAMAGE FOUND ON DOOR HINGE FWD HINGE LOBE AND AFT HINGE LOBE OVALIZED AND OUT OF LIMIT (DIA. 0.355"). REPAIRED WITH BUSHING IAW SRM 52-10-00 FIG 8 VOL 1 AND CMM 52-31-03.
RT WING SEVERE CORROSION ON UPPER BEAVER TAIL. REPAIR CORROSION IAW FEDEX EA 8-5710-103714.
CAC CIRCUMFERENTIAL FRAME AT STA 1099 BETWEEN STRINGER NR 39 LT TO 45 RT EXISTING FRAME REPAIRS AND REPAIRS CHANNEL IN DIF LOCATIONS. REMOVED OLD REPAIR CHANNEL SPLICE AT L NR 52, CUT CAP FRAME AT L NR 41 R. REMOVED SECTION FRAME BTWN L NR 47 L TO 46 R. REMOVED SHEAR CLIPS BTWN L NR 44 R TO 49 R. INSTALLED REPAIR PARTS P/N`S I026182-1A TO -13 IAW SRM 53-30-00-FIG 5 VOL 1, SRM 51-35- 01 VOL 2 AND SRM 51-33-01 VOL 2. SEALING AREA IAW SRM 51-41-02 VOL 2. FABRICATED PARTS IAW DETAIL PART TRAVELER N01182 AND SRM 53-30-00 FIG 5 VOL 1.
CAC 2 EA CRACKS 1.5" LONG AND 3" LONG ON STRIP AT STA 1156 Z= -74 X= -6 AND X= 6. STRIPPED PAINT FROM DAMAGED AREA IAW SRM 51-21-01 PAR C PAG 26 VOL 2. PERFORM NDI CONTROL AND CONFIRMED LENGTH AND END OF CRACK. PERFORMED REPAIR IAW SRM 53-40-00 FIG 17. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027579/N02579 AND IAW SRM 53-40-00, FIG 17 VOL 1.
FOUND FWD LOWER CARGO COMPT, FWD DOOR JAMB AT STA 889 LONGS NR 43 RT AND 40 RT, EXISTING REPAIR AT WEB AND DOOR FRAME. REMOVED WEB REPAIR, FRAME SPLICE REPAIR TWO INTERNAL ANGLE SPLICE AND OPEN WEB AS REQ`D FOR ACCESS IAW SRM 51-30-00 VOL 2. REMOVED AND REPLACED INTERCOSTAL IAW DWG ADA0056. INSTALLED FRAME, ANGLE AND WEB REPAIR IAW SRM 53-50-00 FIG 1 VOL 1 AND DWG ADA0055. FABRICATED PARTS IAW DETAIL PART TRAVELER N01168 AND SRM 53-50-00 FIG 1 VOL 1.
CLG WW FOUND 1 CRACK 1.25" LONG ON HORIZONTAL BULKHEAD BETWEEN STA 1481 AND 1491 X= 30 RT. TRIMMED OUT DAMAGED PORTION OF WEB AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. REPLACED INTERCOSTAL IAW SRM 51-35-01 VOL 1 PAR 1-5. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026749/N01749 IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1.
RT WING LOWER SURFACE AT STA XW 486 ON SKIN TANK BOX FOUND SEVERE CORROSION WITH EXFOLIATION. FASTENERS REMOVED AND REINSTALLED IAW SRM 51-33-01. CORROSION REMOVED IAW SRM 57-10-00 FIG 59 VOL 1 O/B FLAP I/B HINGE SUPPORT REMOVED AND REINSTALLED IAW SRM 51-33-01 VOL 2 PAGE 34/47, EA NR 8-5730-103699 ACCOMPLISHED (SEE JPF).
FOUND FWD CARGO COMPT LONG NR 51 LT AT STA 989 TO STA 1009 EXISTING LONG SPLICE REPAIRS. REMOVED 2 SPLICES IAW SRM 51-30-00 VOL 2. INSTALLED 2 NEW LONGERON SPLICES IAW SRM 53-10-00 FIG 1 AND FIG 2 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER N01190 AND SRM 53-10-00 FIG 1 FIG 2 VOL 1.
RT WING L/E TRACK SUPPORT RIB AT STA XOS 1005 EXISTING REPAIR ANGLE. REMOVED SLAT TRACK DOOR FOR ACCESS IAW MM 57-21-01-2. REPLACED DAMAGED RIB IAW DWG ARB1096. REINSTALLED SLAT TRACK DOOR IAW MM 57-21-01-2.
FOUND LOWER EXT FUSELAGE FOUND DENT 6" BY 4" DEPTH .066" FROM STA 1901 TO STA 1910 LONG NR 33 - 35 RT. DENT EVALUATED AND FOUND TO BE OUT OF LIMITS IAW PROVISION 1A OF SRM 53-20-00 VOL 1 FIG 13. DENTS AREA LESS THAN 3" A PART. REPAIR PERFORMED IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-6.
FOUND LT AND RT WING STRINGER NR 8 FUEL COMPENSATOR FASTENER HOLES OF THE ARB0903 DOUBLER, EXISTING REPAIRS. FOR SUSPECT CRACK STRIP PAINT AREA WITH CHEMICAL METHOD FOR PERFORMED PENETRANT INSP STRIPPED PAINT IAW SRM 51-21-01 PAGE 26 VOL 2. PERFORMED INSP IAW NDTSPM 08 ON EDGE AND SURFACE OF STR NR 8 LT AND RT WING, NO CRACK FOUND. INSPECTED STRINGER NR 8 LT AND RT IAW FEDEX EA NR 8-5720-103624, NO CRACK FOUND.
FOUND AFT LOWER CARGO COMPT FWD JAMB DOOR FRAME, EXISTING REPAIR AT STA 1781 LONG NR 40 TO 42 LT. REMOVED 2 PLATE CONTAINER GUIDE AND 2 SUPPORT LINING SUPPORT AND WEB COVER IAW SRM 51-30-00 VOL 2. PERFORMED GVI, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. ACCOMPLISHED FEDEX EA NR 8-5350-105644 PART 1 INSTRUCTION 1. REINSTALLED REMOVED PART IAW SRM 51-30-00 VOL 2.
RT WING LOWER SURFACE AT XORS 264 ON BEAVER TAIL DOUBLER AROUND NR 15 HEAD FASTENERS FOUND LIGHT CORROSION WITH EXFOLIATION. TAPER LOCKS REMOVED IAW SRM 51-34-01 PAGE 1-7 VOL 2. CORROSION REMOVED IAW SRM 57-10-00 FIG 69 VOL 1, AREA OUT OF LIMITS TRIMMED OUT (SEE JPF). RECOMMENDED ACTION EA NR 8-5710-103696 ACCOMPLISHED.
MAIN CABIN BTWN STA 535 AND 555 X= 90 BTWN HORIZ PRESS PANEL AND FINGER DOUBLER FOUND CORROSION. REMOVED FINGER DOUBLER AND CORROSION IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND SRM 51-21-01 PAR 34. PERF INSP IAW NDTSPM04 FOUND NOM THK.050", MIN .036" IS OUT OF LIMIT. TRIMMED OFF CORRODED WEB AREA IAW EA NR 8-5310-103736. REMOVED PARTS FOR ACCESS. REMOVED THE EXISTING REPAIR PANEL SECTION AND SPLICING, TRIMMED OUT SECTION OF THE P/N NCA6048-3 PANEL, FOUND OLD REPAIR ANGLE ON NCA6048-83 "T" AT STA 535 NOT PERFORMED FOR SRM 53-00-01 FIG 2 SHT 2 VOL 1. CUT OUT DAMAGED AREA IAW SRM 53-00-01 FIG 9. PERFORMED EA NR 8-5310-103736. FAB PART IAW DETAIL PART TRAVELER N01777/I026777 IAW EA NR 8-5310-103736.
FOUND LT AIR CONDITIONING COMPT, SEVERE CORROSION W/EXFOLIATION ON LONGERON FROM STA 560 TO STA 595 X= 28. REMOVED CORROSION IAW SRM 53-10-00 FIG 4 SHT 1 (36 PERCENT). REMOVED FASTENERS ON SKIN, CUT AND REMOVED LONG IAW SRM 53-10-00 FIG 6 VOL 1 AT STA 595. REMOVED FASTENERS ON SKIN AND CLEANED AREA FOR ACCESS TO REINSTALL FASTENERS IS NECESSARY TO REMOVE OR CUT AN SECTION ON FRAME STA 588 IAW SRM 53-10-00 FIG 6 VOL1. REMOVED CORROSION (4.1%) IS IN LIMIT IAW SRM 53-00-01. REMOVED FRAME IAW SRM 51-33-01 VOL 2. REMOVED PARTS AND CUT FRAME IAW DWG ACA0050. INSTALLED NEW SECTION OF LONG NR 48 LT AND REINST FASTENERS ON FRAME IAW SRM 51-33-01 PAGE 34/47 VOL 2. STOP DRILLED ON CRACKED SKIN. FAB NEW DOUBLER AN
FOUND EXTERNAL FUSELAGE AT STA 1219 BTWN LONG NR 51 LT TO 51 RT EXISTING REPAIR DOUBLER. REMOVED EXISTING DOUBLER IAW SRM 51-35-01 VOL2. REPAIRED IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1 AND INSTALLED DOUBLER AND FITTING IAW SRM 51-35-01 PAG 1-13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026042/N01042 AND SRM 53-20-00 FIG 6 VOL 1.
FOUND INTERNAL FUSELAGE AT STA 1250 TO STA 1257 LONGS NR 26 RT AND 27 RT DOOR JAMB FRAME EXISTING DOUBLER REPAIR. PERFORMED INSPECT REPAIR IAW FEDEX EA NR 8-5350-105644 P1, INSTRUCTION 2.
FOUND INTERNAL FUSELAGE AFT MAIN CABIN AT STA 1306 TO STA 1317 LONGS NR 26 RT AND 27 RT DOOR JAMB FRAME EXISTING DOUBLER REPAIR. PERFORMED INSPECT REPAIR IAW FEDEX EA NR 8-5350-105644 P1, INSTRUCTION 3.
MAIN CABIN UPPER LOBE, FOUND CRACK 5" LONG ON FRAME AT STA 1741 LONG NR 13 RT. REMOVED EXISTING SPLICE (L13) AND SHEAR CLIP FROM LONG NR 13 TO NR 9 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME BTWN LONG NR 10 AND NR 9 AND PERFORMED SPLICE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME) DWG AFA0018 REF. INSTALLED EXISTING SPLICE (L13) AND SHEAR CLIP REMOVED PER SRM 51-35-01 AND SRM 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025429/N00429 AND IAW SRM 53-30-00 FIG 5 VOL 1 AND DWG AFA0018.
MAIN CABIN RT SIDEWALL, FOUND NR 1 CRACK 7" LONG ON FRAME AT STA 1781 LONG NR 13. REMOVED EXISTING SPLICE (L13) AND SHEAR CLIP FROM LONG NR 13 TO NR 9 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME BTWN LONG NR 10 AND NR 9 AND PERFORMED SPLICE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME) DWG AFA0030 REF. INSTALLED EXISTING SPLICE (L13) AND SHEARCLIP REMOVED PER SRM 51-35-01 AND SRM 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026541/N01541 AND IAW SRM 53-30-00 FIG 5 VOL 17 DWG AFA0030.
FOUND UPPER FUSELAGE EXTERNAL SKIN DENT 1, 5" BY 1" DEPTH 0.040" FROM LONG NR 17 TO LONG NR 18 RT SIDE AT STA 1621. ACCOMPLISHED FUSELAGE PLATTING REPAIR AT FUS STA 1621 LONG NR 17-18 RT IAW SRM 53- 20-00 FIG 6 SHT 3-4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025032/N00032 AND IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1.
RT INBD FLAP, FOUND FITTING ITEM 665 WITH NR 4 ROLLERS BOLTS HOLES WITH CORROSION REF IPC 27-51-10-01 VIEW F. REMOVED SUPPORT IAW SRM 51-31-01 VOL 2 PAR 6-10. REMOVED CORROSION AND CORROSION LOCAL BLEND IAW SRM 51-21-01 VOL 2 PAR 34D AND IAW SRM 57-20-00 FIG 19 VOL1. REWORKED HOLES ON COUNTERSINK AREAS MAX DIA ON TOP IS 1.279/1.338. FABRICATED AND INSTALLED REPAIR BUSHING IAW EA NR 8-5750-103683 AND SRM 57-20-00 FIG 19 VOL 1. INSTALLED SUPPORT IAW SRM 51-31-01 VOL 2 PAR 6-10.
FWD CARGO COMPT SUMP AREAS, CHANNEL WITH CRACK BTWN STA 879 AND STA 899, Z= -70, X=-5.5. TRIMMED OUT CHANNEL SECTION, BTWN STA 899-879 AND INSTALLED NEW SECTION IAW SRM 53-70-00 VOL 1 FIG 7 SHT 3. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01660 AND SRM 53-70-00 VOL1 FIG 7 SHT 3.
INTERNAL FUSELAGE AFT MAIN CABIN AT STA 1306 TO STA 1317 LONGS 26 LT AND 27 LT DOOR JAMB FRAME FOUND EXISTING DOUBLER REPAIR. PERFORMED GVI ON REPAIR NOT IN COMPLIANCE WITH EO NR 8-5100-7-5001 P2 AND REPAIR FASTENERS WITH SRM 53-50-00 FIG 19 SHT 2 VOL 1. REMOVED EXISTING DOUBLER IAW SRM 51-30-00 AND INSTALLED NEW REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026147/N01147 AND IAW SRM 53-50-00 VOL1 FIG 19.
NLG WW NOSE GEAR BEAM SUPPORT WEB AT STA 570 TO 577 Z= -40 RT SIDE, EXISTING DOUBLER WEB REPAIR. REMOVED AND SCRAPED REPAIR DOUBLERS AND STIFFENER IAW SRM 51-30-00 VOL 2, STRIPPED PAINT IAW SRM 51-21-01 VOL2 PAG 26. PERFORMED NDI SPM 06, FOUND 7 CRACKS. TRIMMED OUT CRACKS AND INSTALLED FILLER, DOUBLERS, NEW NCA6046-116 STIFFENER IAW DWG NCA6046 AND SRM 53-30-00 FIG 6 SHT 3. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01210/I026210 -3, -5, -11 IAW SRM 53-30-00 VOL1 FIG 6 SHT 2, 3, 10.
XORS 402 UPPER BULKHEAD CAP IS CRACKED BELOW STR NR 15, NR 3 TANK. ACCOMPLISHED EA NR 8-5710-99377.
RT WING O/B FLAP UPPER SKIN AT STA XOF 563 AND STA XOF 569 EXISTING DOUBLERS REPAIR. REMOVED NR 4 DOUBLERS IAW SRM 51-30-00. REMOVED T/E SECTION IAW CMM 57-52-02. AFTER REMOVED DAMAGED SKIN FOUND RIB P/N ARC1905-4 WITH CRACK 2" LONG. PERFORMED HFEL INSP IAW NDT SPM 06 AND NO CRACK FOUND. PERFORMED REPAIR DAMAGED AREA IAW SRM 57-10-00 FIG 7 VOL 1 AND REINSTALLED T/E PANEL IAW CMM 57-52-02, SEALED T/E PNL IAW SRM 51-41-01 VOL 2.
AFT MAIN CABIN AFT RT OUTBD SEAT TRACK, EXISTING SPLICE REPAIR BETWEEN STA 1853 TO 1871 X= -100 APPROX PERFORMED GVI IAW EO 8-5100-7-5001 P2 CRITERIA, FOUND CORROSION WITH EXFOLIATION AROUND HEADS OF FASTENERS ON SPLICE SEAT TRACK. REMOVED FASTENERS IAW SRM 51-30-00 VOL 2. REMOVED CORROSION AND VERIFIED LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. NOMINAL THK IS .132, RESIDUAL THK IS .122, MTRL REMOVED IS .010, MAT REMOVED IS 7.5 PERCENT. TREATED REWORKED AREA IAW SRM 51-21-01 VOL 2 AND REINSTALLED FASTENERS IAW SRM 53-70-00 FIG 6 VOL1 AND SRM 51-30-00 VOL 2, MAT REMOVED IS WITHIN LIMITS IAW SRM 53-70-00 FIG 5 VOL 1.
RT WING I/B FLAP LOWER SKIN FWD I/B OF HINGE AT STA XIFH 255, EXISTING DOUBLER REPAIR. NEW REPAIR INSTALLED IAW SRM 57-10-00 FIG 86 VOL 1. RUB STRIP INSTALLED IAW DWG ARC3007. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01106 AND SRM 57-10-00 VOL1 FIG 86 AND DWG ARC3007. REINSTALLED PNL IAW MM 20-50-02.
RT WING L/E AT NR 4 CUTOUT SLAT TRACK, EXISTING DOUBLER REPAIR (LOWER AREA) XIS 286. AT NR 4 CUTOUT SLAT TRACK EXISTING DOUBLER REMOVED AND INSTALLED NEW IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01117 AND SRM 57-10-00 VOL1 FIG 68.
FWD CARGO COMPT AT STA 939 X= 38 EXISTING ANGLE REPAIR IN FLOORBEAM. REMOVED CHANNEL AS REQUIRED IAW SRM 51-30-00 VOL 2, CUTTED FLOORBEAM AT X= 22. INSTALLED REPAIR IAW SRM 53-60-01 FIG 3 VOL 1. REINSTALLED CHANNEL IAW SRM 51-30-00 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01198 AND SRM 53-60-01 VOL1 FIG 3.
CTR CARGO COMPT SUMP AREA FOUND SEVERE CORROSION ON BEAM AT STA 1721 LONG NR 45 LT. REMOVED CORROSION IAW SRM 51-21-01 VOL 2 PAR 34. MAX REMOVED IS .056", REMAINING MAT IS .035", PERCENT REMOVED IS 61 PERCENT, ORIGINAL THK .091". OUT OF LIMITS IAW SRM 53-15-01 VOL 3 FIG 6 AND SRM 53-00-01 VOL 1 FIG 1B. VERIFIED BY NDT INSPECTION SEE JPF. FAB AND INSTALLED NEW PART IAW SRM 53-60-01 VOL 1 FIG 3. REPLACED FASTENERS IAW SRM 51-35-01 AND SRM 51-33-01 VOL 2. REPROTECTED AREA IAW SRM 51-21-01 VOL 2 PAR 31-24.
RT MLG W/W FOUND 1 CRACK 2" LONG ON FRAME AT STA 1505 X= 96. REPLACED FRAME IAW SRM 51-35-01 VOL 2 AND DWG AEA0439 WITH NEW P/N AEA0439-4.
LT WING SLAT NR 2 SCRATCH ON L/E SKIN FROM STA XIS 247 TO STA XIS 258. REPAIRED CARRIED OUT IAW SRM 57-10-00 VOL 1 FIG 43 AND SRM 57-10-00 VOL 1 FIG 29. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00269 AND SRM 57-10-00 VOL1 FIG 29.
LOWER EXT FUSELAGE FOUND DEEP DENT 13" BY 4" MAX DEPTH .200" LOWER SKIN AT STA 899 FROM LONG NR 50 RT TO LONG NR 52 C/L. REMOVE DOUBLER AAU7010-3 AND DOOR ADA8067-1 IAW SRM 51-30-00 VOL 2. TRIMMED OUT DAMAGED AREA AND REMOVED EXISTING REPAIR AT STA 899 LONG NR 51L IAW SRM 53-20-00 FIG 6 SHT 3, 4 VOL 1. PERFORMED HFEC INSP IAW NDT SPM 06, NO CRACK FOUND. INSTALLED REPAIR PARTS P/N I025213-3 TO -19 IAW SRM 53-20-00 VOL1 FIG 6 SHT 3, 4. REINSTALLED AAU7010-3 AND AADA8067-1 IAW SB 53-86 PAGE 12, 13 VIEW A-A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00213 AND SRM 53-20-00 VOL1 FIG 6 SHT 3, 4.
AFT CARGO COMPT AREA FOUND SEVERE CORROSION ON TRACK BETWEEN STA 1871 AND 1801 X=20 RT. REMOVED CORROSION IAW SRM 51-21-01 VOL 2 PAR 34. REMOVED 0.059" AT BS 1821 RT MAX ALLOWABLE IS .025" IAW SRM 53-70-00 VOL1 FIG 5, SHT 1 AND 2 NOTE 3. REMOVED .040" AT BS 1830, REMAINING MAT IS .050", MINIMUM REQUIREMENT IS .060" IAW SRM 53-70-00 VOL1 FIG 5 SHT 1 AND 2 NOTE 8. REPAIR PERFORMED IAW SRM 53-70-00 VOL 1 FIG1 SHT 3 AND 4 (NEW SEAT TRACK SECTION INSTALLED). FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00372/I025372 AND SRM 53-70-00 VOL1 FIG 1 SHT 3-4.
CTR CARGO COMPT BILGE FOUND CORROSION WITH EXFOLIATION ON SKIN BTWN STA 1521 AND STA 1541 FROM LONG NR 45 RT TO LONG NR 42 LT. TRIMMED OUT DAMAGED SKIN AND REPAIRED IAW SRM 53-20-00 VOL 2 FIG 6 SHT 15. FABRICATED PARTS IAW ETAIL PARTS TRAVELER I026602/N01602 AND IAW SRM 53-20-00 VOL1 FIG 6 SHT 3-6.
LT WING INBD FLAP: DENTS ON LOWER SKIN AFT PANEL AT STA XIFH 171, XIFH 177 AND XIFH 201 WITH DEFORMATION OF BACK-UP STRUCTURE. PERFORMED REPAIR SKIN IAW SRM 57-10-00 FIG 3 VOL 1 IAW SRM 51-41-01 FIG 1 VOL 2. REPLACED TEE IAW SRM 51-35-01 PAG 1/13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027615/N02615 AND SRM 57-10-00 VOL1 FIG 3, DWG ARC2481 (-5) AND ATM P0208753.
MAIN CABIN DEEP WEAR ON SEAT TRACK AT STA 1521 X= -27 REF J/C 5300E290-1J. INSTALLED SEAT TRACK SECTION WITH SPLICE AT STA 1531 IAW SRM 53-70-00 FIG 1. FABRICATED PART IAW DETAIL PART TRAVELER N01369 AND SRM 53-70-00 VOL1 FIG 1.
MAIN CABIN DEEP WEAR ON SEAT TRACK BETWEEN STA 1721 AND 1741 X= -27. REF J/C 5300E290-1J. INSPECTION PERFORMED AND FOUND SEAT TRACK NOMINAL THK NOT TO BE WITHIN LIMITS IAW SRM 53-70-00 PAGE 22. SEAT TRACK REPAIR IS PERFORMED SEAT TRACK IS CUT AT STA 1711 AND 1751 IAW SRM 53-70-00 FIG 1. TRIMMED NEW FABRICATED SECTION IAW DETAIL PARTS TRAVELER I026368 AND SRM 53-70-00 FIG 1. INSTALLED NEW SEAT TRACK SECTION AND 2 SPLICES IAW SRM 53-70-00 FIG 1.
LWR EXT FUSELAGE FOUND NR 3 DEEP DENTS 15" BY 4" MAX DEPTH .090" FROM STA 979 TO STA 967 FROM L39 RT TO 42 RT. REMOVED 2 EXISTING REPAIRS BTWN STA 999 TO STA 959 FROM L#38 TO #42 RT IAW SRM 51-33-01 VOL2 P34/47. TRIM OUT DENTS AREA WITHOUT CUT INNER DOUBLER. PERFORMED INSP IAW NDT SPM06, NO CRACK FOUND. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-00 VOL 1 FIG 6 AND SRM 53-50-00 VOL1 FIG 26. IN ORDER TO PERFORM REPAIR, REMOVED AND INSTALLED SCUFF PLATE IAW SRM 51-31-01 VOL2 PAGE 36/41. CLEANED SCUFF PLATE AREA AND TREAT REPAIR AREA IAW SRM 51-21-01 VOL 2 PAR 22. SEAL SCUFF PLATE IAW SRM 51-41-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00219 AND SRM 53-20-00 VOL1 FIG 6 AND SRM 53-50-00
FWD CARGO COMPT BILGE MODERATE CORROSION ON CAP FRAME AT STA 879 LONG NR 50 LT TO LONG NR 51 LT. REMOVED EXIST REPAIR SPLICE FOR ACCESS, REMOVED CORROSION, MTL REMOVED IS OUT LIMITS. INSTALLED A REPAIR CAP SECTION BTWN LONG NR 47 LT TO LONG NR 47 RT IAW SRM 53-30-00 VOL 1 FIG 8. INSTALLED A REPAIR SPLICE BTWN LONG NR 48 RT AND LONG NR 47 RT IAW SRM 53-30-00 VOL 1 FIG 8. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01646 AND SRM 53-30-00 VOL1 FIG 8.
LOWER EXT FUSELAGE, FOUND DEEP DENT 3" BY 1,5" MAX DEPTH .065" AT STA 1781 FROM L 44 LT TO L 45 LT. TRIMMED OUT DAMAGED SKIN, REPAIRED IAW SRM 53-20-00 VOL1 FIG 6 SHT 2A-4. PERFORMED NDT INSPECTION NO CRACK FOUND, FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025223/N00223 IAW SRM 53-20-00 VOL1 FIG 6 SHT 3-4.
AFT CARGO COMPT AREA FOUND CORROSION WITH EXFOLIATION ON BEAM AT STA 1902 BTWN X=0 CTR & X= 20 LT. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 8. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025371/N00371 IAW SRM 53-30-00 VOL1 FIG 5 AND SRM 53-00-01 VOL 1 FIG 8.
RT INBOARD ELEVATOR FOUND DEEP DENT 2" BY 2" MAX DEEP .080" ON UPPER SKIN FROM STA XH 153 TO XH 158. REPAIRED SKIN IAW SRM 57-00-01 VOL 1 FIG4 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025079/N00079 AND IAW SRM 57-00-01 VOL1 FIG 14 SHT 2.
LT INB FLAP FOUND FITTING ITEM 665 WITH NR 3EA HOLES WITH CORROSION REF IPC 27-51-10-01 VIEW F. REMOVED SUPPORT IAW SRM 51-31-01 VOL 2 PAG 6-10. REMOVED CORROSION AND CORROSION LOCAL BLEND IAW SRM 51-21-01 VOL 2 PAR 34A AND IAW SRM 57-20-00 VOL 1 FIG 19. REWORKED HOLE ON COUNTER SINK AREA MAX DIA ON TOP IS 1,279. FABRICATED AND INSTALLED A REPAIR BUSHING IAW EA NR 8-5750-103681. INSTALLED SUPPORT IAW SRM 51-31-01 VOL 2 PART 6-10.
RT WING TIP WING LOWER SKIN TWO DOUBLERS REPAIR O/B OF ACCESS DOOR XFS 1191. REMOVED AND REPLACED STIFFENER IAW DWG ARB2204 ARB1044. INSTALLED DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL 1. FABRICATED PART IAW DETAIL PARTS TRAVELER N01124 AND SRM 57-00-01 FIG 4 SHT 2 VOL 1.
LOWER EXT FUSELAGE FOUND DENT 5" BY 4" DEPTH .030" FROM STA 1801 TO STA 1810 L50-51 RT. DENT DIMENSIONS MEASURED PER SRM 53-20-00 VOL 1 FIG 1 B SHEET 2 STEP 1 AND FOUND TO BE OUT OF LIMITS, PROVISION 1A NOT MET DENTS ARE 1" A PART, MINIMUM REQUIREMENT IS 3". REFER TO JPF FOR REPAIR. REMOVED EXISTING DOUBLER, INSTALLED REPAIR PARTS IAW SRM 53-20-00 VOL1 FIG 6 SHT 3.4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00232 AND SRM 53-20-00 VOL1 FIG 6 SHT 3.4.
XORS 346 LWR BULKHEAD CAP IS CRACKED HORIZONTALLY THRU THE LUG AT STR 44. CUT LOWER VERTICAL LEG FLUSH TO HORIZONTAL LEG TO COMPLETLY REMOVE CRACK AND INSTALLED "T" REPAIR IAW SRM 57-20-00 VOL1 FIG 27 SHT 2.
LOWER FUS EXT SKIN MODERATE PITTING CORROSION FROM STA 1099 TO STA 1521 FROM L 48 LT TO L 48 RT. REPAIRED AREA STA 1268 AND STA1329 IAW SRM 53-40-00 FIG 20 SHT 1&4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01728/I026728 IAW SRM 53-40-00 FIG 20 SHT 4 VOL 1.
INBOARD LT ELEVATOR FOUND 5 DENT 1" BY 1" MAX DEEP 0.070" AND FROM STA XE 136 TO XE 211.477. REPAIRED SKIN IAW SRM 55-10-00 FIG 8 AND SRM 55-10-01 VOL 1 FIG 3 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025070/N00070 AND SRM 55-10-00 VOL 1 FIG 7.
LT WING INT AILERON FOUND CORROSION UNDER SKIN AILERON LOWER SIDE SKIN AT STA 300 XIA. CUT DAMAGED SECTION OF LOWER SKIN. REPAIRED IAW SRM 57-10-00 FIG 86 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027611/N02611.
RT WING L/E INT STRUCTURE FOUND 1 CRACK 1.25" LONG ON RIB AT STA XORS 536. REPAIRED CRACK IAW SRM 57-00-01 FIG 10 SHT 1-4 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER N02608/I027608 IAW SRM 57-00-01 FIG 10 SHT 1VOL 1.
LOWER FUSELAGE EXT SKIN FOUND 1 DENT .50" BY .50" MAX DEEP .070" AT STA 340 LONG NR 28 RT SIDE. REMOVED SCUFF PLATE IAW MM 20-50-02. REMOVED SEALANT, PREP AND TREATED AREA IAW SRM 51-21-01 VOL 2 PG 21-25. CUT OUT DAMAGED SKIN AREA IAW SRM 53-20-00 SHT 3-4 FIG 6 VOL 1. PERFORMED HIGH FREQ EDDY CURRENT INSPECTION IAW NDTSPM 06, NO CRACK FOUND. REPAIRED AREA IAW SRM 53-20-00 SHT 3-4 FIG 6 VOL 1. REINSTALLED SCUFF PLATE IAW MM 20-50-02 WEATHER SEALING AREA IAW SRM 51-42-01 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER I027041/N02041 AND SRM 53-20-00 SHT 3-4 FIG 6 VOL 1.
RT WING L/E XOS 550 1 CRACK ON ATTACHED PANEL STRAP. LOWER LEADING EDGE STRINGER DOUBLER REPAIRED IAW SRM 57-10-00 FIG 49, PAGE 163 VOL1. FAB PART IAW DETAIL PART TRAVELER N02724 AND SRM 57-10-00 FIG 49 VOL 1.
UPPER FWD RUDDER REAR SPAR STRUCTURE, SEVERE CORROSION WITH EXFOLIATION ON WEB. REMOVED HINGE TO GAIN ACCESS AND REPAIRED DAMAGED WEB IAW SRM 55-00-01 FIG 9 VOL 1 AND REINSTALLED. REMOVED HINGE PER SRM 51-31-01 PAGE 36/41. FAB PART IAW DETAIL PART TRAVELERS N02420 AND SRM 55-00-01 FIG 9 VOL 1.
COCKPIT STA 340.00 X = 50 TO X = 60 REF SP10350036 DURING INSTALLATION OF S43894- 00A1 CLIP FOUND CRACK LONG NR .500" ABOUT ON WEB AND 4 HOLES WITH .250" DISTANCE ON WEB AND CAP. SEE ATTACHED SHT. REPAIRED CRACK IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. PLUGGED HOLES SEPARATELY WITH AD MATERIAL AND INSTALLED STRAP IAW DWG SP11530083. FABRICATED PART DETAIL PARTS TRAVELER NR I026490/N01490 IAW SRM 53-00-01 FIG 4 SHT 2, AND DWG SP11530083.
LOWER EXT FUSELAGE FOUND 3 DEEP DENT (NR 1: 4" BY 3" DEPTH .032", NR 2: 3" BY 2" DEPTH .100", NR 3: 4" BY 1.5" DEPTH .110") FROM STA 1741 TO STA 1751 FROM LONG NR 39 LT TO LONG NR 41 LT. TRIMMED OUT DAMAGE AREAS PERFORMED NDT INSPECTION ON INNER DOUBLER NO CRACK FOUND. REPAIRED IAW SRM 53-20-00 VOL 1 FIG 6 SHT 2-4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025221/N00221 IAW SRM 53-20-00 VOL 1 FIG 6 SHT 2-4 AND SRM 53-30-00 VOL 1 FIG 10. INSTALLED NEW SHEAR CLIP AND STRAP IAW SRM 53-30-00 VOL 1 FIG 10.
UPPER FUSELAGE, LEFT SIDE, INTERNAL ON FRAME AT STA Y=1721, LONG NR 13, FOUND NR 1 CRACK 5" LONG. REMOVED EXISTING SPLICE AND SHEAR CLIP FROM LONG NR 13 TO 19 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME FROM LONG NR 10 TO LONG NR 9 AND PERFORMED SPLICE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME), DWG AFA0019 (REF). INSTALLED EXISTING SPLICE ( LONG NR 13) AND SHEAR CLIP REMOVED IAW SRM 51-35-01 AND 51-33-01VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025535/N00535 IAW SRM 53-30-00 FIG 5 VOL 1 AND DWG AFA0019.
MAIN CABIN UPPER LOBE CRACK 5" LONG ON FRAME AT STA 1721 LONG NR 13 RT. REMOVED EXISTING SPLICE (LONG# 13) AND SHEAR CLIP FROM LONG NR 13 TO LONG NR 9 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME BETWEEN LONG NR 10 AND LONG NR 9 AND PERFORMED SPLICE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME), DWG AFA0019 (REF). INSTALLED EXISTING SPLICE (LONG NR 13) AND SHEAR CLIP REMOVED IAW SRM 51-31-01 AND 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025428/N00428 IAW SRM 53-30-00 FIG 5 VOL 1 AND DWG AFA0019.
RT WING L/E SKIN AT NR 10 CUTOUT SLAT TRACK, EXISTING DOUBLER REPAIR STA XOS 659. RT WING L/E SKIN AT SLAT TRACK NR 10 EXISTING DOUBLER REPAIR STA XOS 659 REMOVED IAW SRM 51-30-00 VOL 2 AS NONE CONFIRMING REPAIR. REPLACED WITH DOUBLER IAW SRM 57-10-00 FIG 68. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01119 AND SRM 57-10-00 FIG 68 VOL 1.
RT WING L/E AT NR 9 CUT OUT SLAT TRACK LWR AREA, EXISTING DOUBLER REPAIR XOS 602. EXISTING REPAIR REMOVED, AREA ASSESSED TWO CRACKS TRIMMED OUT AND FILLERS FABRICATED, NEW DOUBLER PLATE FABRICATED AND FITTED IAW SRM 57-10-00 PAGES 215-216A FIG 68 (SHT 1,2,3) VOL 1. EDGES FAIRED WITH PR1422 B2 IAW SRM 57-10-00, PAGE 215, FIG 68, SHT 1, VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01118 AND SRM 57-00-00, FIG 68, VOL 1.
CTR CARGO COMPT SUMP AREA FOUND SEVERE CORROSION ON BEAM AT STA 1741 BTWN LONG NR 46 RT AND LONG NR 46 LT. TRIMMED OUT DAMAGED PORTION OF HORIZONTAL LEG OF BEAM AND REPAIRED IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026571/N01571 IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.
CLG W/W FOUND 1 CRACK 1" LONG ON HORIZONTAL BLKHD BTWN STA 1441 AND STA 1431 X = 30 RT. TRIMMED OUT DAMAGED PORTION WEB AND INSTALLED FILLER AND RETAINER DOUBLER IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026748/ N01748 IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1.
LOWER EXT FUSELAGE FOUND 3 DEEP DENT (NR 1: 1,5" BY 3" DEPTH .080", NR 2: 1" BY 1" DEPTH .075", NR3: 1,5" BY 1, 5" DEPTH .040" ) NICK AND SCRATCH FROM STA 959 TO STA 979 FROM L31 RT TO L34 RT. TRIMMED OUT DAMAGED SKIN WITHOUT CUT INTERNAL DOUBLER IAW SRM 53-50-00 VOL 1 FIG 26 SHT 3. PERFORMED HFEC INSP IAW NDT SPM 06, NO CRACK FOUND. INSTALLED REPAIR IAW SRM 53-50-00 VOL 1 FIG 26 SHT3-5 ( STEP 14A ). FABRICATED PARTS IAW DETAIL PART TRAVELER N00220 AND IAW SRM 53-50-00 FIG 26 SHT 3 VOL 1.
RT WING L/E SKIN AT NR 13 CUT OUT SLAT TRACK LOWER AREA, EXISTING DOUBLER REPAIR XOS 832. RT WING L/E SKIN AT NR 13 LOWER SLAT TRACK AT XOS 832 REMOVED NON CONFORMING REPAIR AND REPLACED WITH DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FAB PART IAW DETAIL PART TRAVELER N01120 AND SRM 57-10-00 FIG 68 VOL 1.
LOWER EXT FUSELAGE FOUND 1 CRACK 1" LONG AT STA 1039 L46 LT. TRIMMED CRACKED AREA AND INSTALLED INTERNAL DOUBLER AND SKIN PLUG IAW SRM 53-20-00 FIG 13 SHT 9 VOL 1. TRIMMED AND REMOVED FOR ACCESS SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1. REPAIRED AND INSTALLED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER N00215 AND SRM 53-20-00 FIG 13 SHT 9 VOL 1 AND SRM 53-30-00 FIG 10 VOL 1.
RT WING INBOARD AILERON SEVERE CORROSION ON UPPER AND LOWER SKIN. REMOVED UPPER AFT CORRODED SECTION OF SKIN AND REPAIRED PER SRM 57-10-00 FIG 85 VOL 1. REMOVED FWD, CTR UPPER CORRODED SECTION OF SKIN AND REPAIRED PER SRM 57-10-00 FIG 85 VOL 1. FWD AND AFT SECTION LOWER CORRODED SKINS REMOVED, FOR INSP WILL BE REPAIRED WITH NRC N02620. FAB PART IAW DETAIL PART TRAVELER N01529 AND SRM 57-10-00 FIG 85 VOL 1 (INBOARD AILERON WILL BE INSTALL WITH NRC N02620).
LOWER EXT FUSELAGE FOUND DEEP DENT 4" BY 2", MAX DEPTH .100" AT STA 999 FROM L 36 LT TO L 35 LT. REPAIRED DENT IAW SRM 53-20-00 FIG 13 SHT 2, 2A, 5 AND 14 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N00217 AND SRM 53-20-00 VOL 1.
RT AIR COND COMPT FOUND 1 CRACK 2" LONG ON HORIZ BLKHD AT STA 495 X = -24. REMOVED EXISTING REPAIR IAW SRM 51-33-01 VOL 2. CUT OUT CRACKED AREA AT SUPPORT BEAM WEB. INSTALLED NEW PARTS IAW SRM 53-30-00 FIG 6 VOL 1 COMBINING DETAIL "E" AND "J" VOL 1. REINSTALLED OLD SHIM UNDER ACA 3837 FITTING. FABRICATED DETAIL PARTS TRAVELER NR N02007/I027007 IAW SRM 53-30-00 FIG 6 VOL 1.
FWD CARGO COMPT BILGE CRACK .50" LONG ON SHOVEL CLIP STA 595 L 51 LT. REPLACED SHOVEL END IAW DWG NCA6014. (WORKED IN CONJUCTION WITH NRC# N01651).
FWD CARGO COMPT BILGE CRACK 2" LONG ON SHEAR CLIP STA 595 L 49 LT TO GAIN ACCESS. REMOVED SPLICE FRAME NR 47 LT STA 615. REMOVED SHEAR CLIP AND SUPPORT ACA0054 (REF) AS NECESSARY IAW SRM 51-33-01 AND 51-35-01 VOL 2. REPLACED SHOVEL END IAW DWG NCA6014. REINSTALLED REMOVED PARTS FOR ACCESS IAW SRM 51-33-01 AND 51-35-01 VOL 2.
LT WING OUTBD AILERON AT STA XOA 876 ON UPPER SKIN EXT FOUND BULGE AND SUSPECT CRACK. ACCOMPLISHED UPPER SKIN LOCAL DAMAGE REPAIR IAW SRM 57-10-00 FIG 56 VOL 1 PG 187. THE BALANCE WILL BE ACCOMPLISHED WITH NRC N00023. FABRICATED PART IAW DETAIL PART TRAVELER N01860 AND IAW SRM 57-10-00 FIG 56 VOL 1.
RT WING CUTOUT SKIN AT SLAT TRACK STA XOS 550 LOWER AREA, EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR REMOVED, AREA ASSESSED. CRACK TRIMMED OUT AND FILLER MANUFACTURED. NEW DOUBLER FABRICATED AND FITTED IAW SRM 57-10-00 FIG 68 VOL 1 PAGE 215. EDGES OF DOUBLER PLATE SEAL FAIRED IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1 PAGE 215.
CAC: SUSPECT CORROSION BETWEEN DIFFERENT MATERIAL (SKIN AND INTERNAL DOUBLER ) AT STA 1139 FROM L 43 RT TO L44 RT. REMOVED SHEARCLIP AND CAP FROM L NR 38 RT TO L NR 51 LT, IAW SRM 51-35-01 AND IAW SRM 51-33-01 VOL 2. CUT TEARSTRIP FROM L NR 43-L NR 45 RT. REMOVED CORROSION ON SKIN, RESIDUAL MTL THK IS OUT LIMITS. REPAIRED SKIN IAW SRM 53-20-00 FIG 6 SHT 3 VOL 1. REINSTALLED SHEARCLIP AND CAP IAW SRM 51-35-01 AND SRM 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PART TRAVELER N01584 AND SRM 53-20-00 FIG 6 VOL 1.
LT AIR COND COMPT: WEARS ON FRAME AT STA 588 X = 62. BLENDED OUT WEARS IAW SRM 53-00-01 VOL 1 FIG 1B, PERFORMED INSPECTION IAW NDI SPM 04 MIN THK .054" NOM. .063" MAT IS WITHIN LIMITS IAW SRM 53-00-01 VOL 1 FIG 1B. PROTECTED AREA IAW SRM 51-21-01 VOL 2 PAR 22. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026996 AND IAW SRM 53-30-00 VOL 1 FIG 4A.
RT WING INB'D AILERON CORROSION WITH EXFOLIATION ON LOWER SKIN AILERON (FINGER DOUBLER AND SKIN ). REMOVED DAMAGED SECTION OF SKIN AND REPAIRED X SRM 57-10-00 FIG 86 VOL 1. FAB PART IAW DETAIL PART TRAVELERS X SRM 57-10-00 FIG 86 VOL 1 AND N02620 AND SRM 57-51-01 FIG 1 VOL 3. FAB AND INST NEW SECT OF DOUBLER (1 THK ONLY) IAW SRM 57-10-00 FIG 85 VOL 1.
LWR FUSELAGE EXT SKIN FOUND DEEP DENT 2" BY 3" DEEP .12" AT STA 449 LONG NR 36 RT. INSTALLED FINGER DOUBLER TITANIUM IAW SRM 53-20-00 FIG 13 SHT 2A SHT 5 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NR I025117/N00117 AND IAW SRM 53-20-00 VOL 1.
UPPER FUSELAGE EXTERNAL SKIN DENT 1.5 INCH BY 1 INCH DEPTH .062" AT STA 1069 FROM L12 TO L13 RT SIDE. ACCOMPLISHED FUSELAGE PLATING REPAIR AT STA 1069 LONG 12-13 RT IAW SRM 53-20-00 FIG 6 SHT 3 -4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00185/I025185 IAW SRM 53-20-00 FIG 6 VOL 1.
LT WING INT L/E FOUND 2 DEEP WEAR ON SUPPORT TRACK NR 6. BLENDED OUT AREAS OF SUPPORT IAW SRM 57-00-01 PAGE 1 FIG 14 VOL 1. RECORDED MATERIAL REMAINING ON REWORKED AREAS (AREA 1 .8751" ) AND ( AREA 2 .580" ), NOM THK OF DAMAGES AREA IS 1" IAW DWG ARB1200. BLEND OUT IS .1249" AND 0.020", THE BLENDED OUT IS 12% AND 2% SO THE BLEND OUT IS WITHIN LIMITS BECAUSE THE MAX IS 20% IAW SRM 57-00-01 FIG 1A VOL1. REPROTECTED AREAS IAW SRM 51-21-01 PAG 21-25 VOL 2 AND INSTALLED MISSING BLOCK PROTECTION P/N ARB1180-1 IAW DWG ARB0186.
LOWER EXT FUSELAGE FOUND CRACK .75" LONG ON AFT UPPER CORNER AIR CONDITIONING COMPT RT SIDE ( WITH DRILL STOP). REPAIRED IAW SRM 53-50-00 VOL1 FIG 3 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025283/N00283 IAW SRM 53-50-00 VOL1 FIG 3.
LOWER EXT FUSELAGE FOUND 2 DEEP DENT (NR1: 1" BY 1.75" DEPTH .125", NR 2: 1" BY .75" DEPTH .040") ON SKIN AT STA 1997 FROM L49 LT TO L50 LT. TRIMMED OUT DAMAGED AREAS REPAIRED IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-6 AND IAW SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025224/N00224 IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-6.
LOOP-A ENG NR 1 ILLUMINATED IN FLIGHT, RAN ORH, DETERMINED LOOP-A SHORTED, NO FIRE. FOUND P1-8015 WIRE CHAFING ON CHANNEL STRUCTURE. REPOSITION CLAMP AND CHECKED WIRE TO BE OKAY. INSTALLED VULCANIZED TAPE OVER AREA. SMWP 20-00-06. OPS CHECK GOOD IAW MM 26-11-00.