N780FD
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.
108 reports on file, 2014-07-22 – 2021-11-27.
Part: FILTER — DIRTY · airframe 77,793 hrs · 30,561 cycles
"MAIN CARGO FIRE" MESSAGE ON EICAS ON LANDING ROLL OUT. EMER EVAC OFF THE END OF THE RUNWAY. EMERGENCY DECLAERED. SHGN 27NOV21 04:44 ROC U WHEN ARRIVING AT A/C A WALK AROUND WAS PERFORMED. FOUND SAND AND DEBRIS ON BELLY OF A/C FORWARD OF ACM INLETS, INSIDE ACM INLETS AND LOWER WING SURFACE INBOARD OF PYLONS. AIRCRAFT SYSTEMS OPERATED NORMALLY DURING MAINTENACE TAXI AND ENGINE RUNS. REF MM05-51-56-2 SMOKE OR FUMES IN CABIN MAINTENANCE PRACTICES. PERFORMED 2 MINUTE HIGH POWER RUNS PER JRH TO EPR OF THE DAY. BOTH ENGINES PERFORMED NOMINALLY WITH ACCEPTABLE PARAMETERS. REF MM21-00-01-3 SMOKE OR FUMES TROUBLESHOOTING, ENGINE RUNS & OPERATIONAL TESTS SHOWED NO SMOKE OR FUMES IN CABIN. BOTH PACK SYSTEMS OPERATED NOMINALLY. REPLACED HEPA FILTER AFTER ENGINE RUNS PRECAUTIONARY REF MM21-25-02-4. A/C OK TO CONTINUE.
Part: SLIDE — UNKNOWN (N/A) · airframe 77,793 hrs · 30,561 cycles
R1 SLIDE DEPLOYED FOR EMERGENCY EVACUATION. REMOVED AND REPLACED R1 DOOR SLIDE PER AMM 25-66-01- 4. A/C OK FOR SERVICE
Part: NONE — NONE (N/A) · airframe 77,776 hrs · 30,553 cycles
PDIS 780 29-02 5877 23NOV21 IND OPEN U L HYD QTY SHGN 23NOV21 08:05 IND U ACFT BLOCKED IN W LEFT HYD SYSTEM QTY READING .55. RAN LEFT SYSTEM ELECTRIC PUMPS AND OPENED MAIN CARGO DOOR AS REQ. W/ NO PUMP CAVITATION. SHGN 23NOV21 08:30 IND U FOUND DPI INDICATOR LEAKING IN LEFT ENGINE DRIVEN PUMP CASE DRAIN PRESSURE FILTER MODULE ASSEMBLY. ORDERED PRESSURE FILTER, RETURN FILTER, DPI INDICATOR, AND ALL ASSOCIATED O-RINGS AND PACKINGS. AIRCRAFT HYD QTY LOSS FROM THE L HYD SYSTEM IN FLT. SHGN 23NOV21 08:30 IND FOUND DPI INDICATOR LEAKING IN LEFT ENGINE DRIVEN PUMP CASE DRAIN PRESSURE FILTER MODULE ASSEMBLY. ORDERED PRESSURE FILTER, RETURN FILTER, DPI INDICATOR, AND ALL ASSOCIATED O-RINGS AND PACKINGS. SHGN 23NOV21 12:35 IND REMOVED DPI FROM LEFT PYLON HYDRAULIC MANIFOLD REF B757 AMM 29-11-17-4. FACT 23NOV21 19:32 IND INSTALLED DPI AS REQUIRED. SERVICED SYSTEM AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. REF. MM. 29-11-17-4.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 77,429 hrs · 30,310 cycles
PDIS 780 29-02 5505 08JUN21 IND OPEN U ON DESCENT HYDRAULIC SYSTEM PRESSURE ILLUMINATED. (L) RAN QRH, LEADING US TO USE ALTN GEAR EXTEND, LE, TE. SHGN 08JUN21 05:48 IND APON SHUT DOWN HYD QTY IN LEFT SYSTEM READ .08. MX FOUND L/H ENGINE DRIVEN HYDRO PUMP HOUSING CRACKED WITH APPROXIMATELY 2 INCH CRACK AT THE 6 :00 POSITION. FACT 08JUN21 22:25 IND FINISHED INSTALL OF #1 EDP REF: AMM 29-11-05-4-2, PERFORMED ENGINE 5 MIN IDLE RUN REF JRH 5-35. OPS CHECK GOOD, LEAK CHECK GOOD. RESERVICED HYD SYS REF: AMM 12-12- 01-3.
Earlier reports · 2014–2020 · 104 reports
2020
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BOAD IN BAY 5L HAS A PUNCTURE IN UPPER SKIN. REPAIRED PUNCTURE ON MAIN CABIN FLOOR BOARD AND APPLIED ANTI-SKID TAPE TO AREA, IAW B757 SRM 53-00-50 FIG 201.
Part: FRAME — CRACKED (ZONE 200) · airframe 76,969 hrs · 30,018 cycles
LT 1640 FRAMA INBOARD FASTENER HOLE AT S14L CRACK INDICATION.
Part: FRAME ANGLE — CRACKED (NR 2 PYLON) · airframe 76,969 hrs · 30,018 cycles
NR 2 PYLON UPPER RT PANEL SUPPORT IS CRACKED APPROXIMATELY STA 156. REPAIRED PER B757 SRM 54-51-71-2R AND 51-70-11-0G FIG 1.
Part: PANEL — CORRODED (LT WING TE) · airframe 76,969 hrs · 30,018 cycles
LT WING UPPER TRAILING EDGE PANEL OUTBOARD OF AILERON IS CORRODED. REPAIRED PER B757 SRM 57-51-01-2R.
Part: SKIN — DENTED (RT ELEVATOR) · airframe 76,969 hrs · 30,018 cycles
RIGHT ELEVATOR LOWER SURFACE IS DENTED 50 INCHES FROM OUTBOARD EDGE AND 6 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR LOWER SURFACE DENT 50" FROM OUTBOARD EDGE AND 6" FROM TRAILING EDGE, IAW FEDEX EA F-5520-T0358329 AND B757 SRM 51-70-17 PARA 4L AND SRM 51-70-03 PARA 5L. F-5520-T0358329-P1 STABILIZERS-ELEVATORS-RT ELEVATOR-ELEV STA 241-LOWER SKIN-DENTED. MAJOR REPAIR
Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 76,969 hrs · 30,018 cycles
MAIN CARGO DOOR CUTOUT FWD LOWER SEAL DEPRESSOR DAMAGED. COMPLIED WITH FEDEX EA F-5310-T0358270-P1 MAINFRAME-SEAL DEPRESSOR-STA 480 AND STA 620-S-16L-DENTED.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 76,969 hrs · 30,018 cycles
DURING AGING AIRCRAFT INSPECTION FOUND LT OUTBOARD AFT FLAP LOWER INBOARD SKIN TO BE DELAMINATED. REMOVED FINISH, EVALUATED, REMOVED DAMAGE, AND REPAIRED LT OUTBOARD AFT FLAP, IAW B757 SRM 57-53-01-2R TABLE 2, 51-70-04-0G PARA 4A-I. MAJOR REPAIR.
Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 76,969 hrs · 30,018 cycles
MAIN CARGO DOOR CUTOUT LOWER SEAL DEPRESSOR DAMAGED. COMPLIED WITH FEDEX EA F-5310-T0358270-P1 FUSELAGE-MAINFRAME-SEAL DEPRESSOR-STA 480 AND STA 620-S16L-DENTED.
Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1663-RBL 54. REMOVED CORROSION, IAW B757 SRM 51-10-02, ORIG MAT .071", REMOVED MAT .003", REMAINING MAT .068". FOUND TO BE WITHIN LIMITS, IAW BOEING DWG 657N4303 REV B AND B757 SRM 53-60-15-1A DETAIL III. TREATED BARE METAL, IAW B757 SRM 51-20-01.
Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1653-BS 1658, LBL 54. REMOVED CORROSION AS REQUIRED, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .071 MATERIAL LOSS OF .002 REMAINING MATERIAL THICKNESS .069. FOUND TO BE WITHIN LIMITS, IAW BOEING DRAWING 657N47303 REV B AND B757 SRM 53-60-15-1A DETAIL IV. RESTORED FINISH, IAW B757 SRM 51-20-01-04.
Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1642-BS 1658, RBL 54. REMOVED CORROSION, IAW B757 SRM 51-10-02, ORIG MAT .071", REMOVED MAT .003", REMAINING MAT .068". FOUND TO BE WITHIN LIMITS, IAW BOEING DWG 657N4303 REV B, B757 SRM 53-60-15-1A, TREATED BARE METAL, IAW B757 SRM 51-20-01.
Part: CLOSEOUT PANEL — DAMAGED (MAIN CARGO DECK) · airframe 76,969 hrs · 30,018 cycles
MCD FWD WEB AND CLOSEOUT PANEL DAMAGED. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED, IAW B757 SRM 51-40-02, B757 SRM 51-40-05, BOEING DWG 69-49309 REV D, TREATED BARE METAL, IAW B757 SRM 51-20-01.
Part: WEB — DAMAGED (MCD) · airframe 76,969 hrs · 30,018 cycles
MCD AFT WEB AND CLOSEOUT PANEL DAMAGED. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED, IAW B757 SRM 51-40-02 B757 SRM 51-40-05, BOEING DWG 69-49309 REV D. TREATED BARE METAL, IAW B757 SRM 51-20-01.
Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
FLOOR PANEL SUPPORT STRUCTURE UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1668, LBL 55. REMOVED CORROSION AS REQUIRED, IAW B757 SRM 51-10-02 ORIGINAL THICKNESS .071. MATERIAL LOSS OF .002, REMAINING MATERIAL THICKNESS .069 FOUND TO BE WITHIN LIMITS, IAW BOEING DRAWING 657N4303 REV B AND B757 SRM 53-60-15-1A DETAIL IV. RESTORED FINISH, IAW B757 SRM 51-20-01-04.
Part: DUCT — CRACKED (FWD CARGO) · airframe 76,969 hrs · 30,018 cycles
FWD CARGO COMPARTMENT RT SIDE AT STA710 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 710 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801.
Part: DUCT — CRACKED (FWD CARGO) · airframe 76,969 hrs · 30,018 cycles
FWD CARGO COMPARTMENT RT SIDE AT STA 670 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 670 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801.
Part: COVER — CRACKED (ZONE 100) · airframe 76,969 hrs · 30,018 cycles
NLG STEERING CABLE PULLY ACCESS COVER IS CRACKED ON THE BOTTOM SURFACE **SDR ENTERED IN ERROR**
Part: COVER — CRACKED (ZONE 100) · airframe 76,969 hrs · 30,018 cycles
**SDR ENTERED IN ERROR** **SDR ENTERED IN ERROR**
Part: DUCT — CRACKED (FWD CARGO) · airframe 76,969 hrs · 30,018 cycles
FWD CARGO COMPARTMENT RT SIDE AT STA 690 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA 690 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801.
Part: DUCT — CRACKED (FWD CARGO) · airframe 76,969 hrs · 30,018 cycles
FWD CARFO COMPARTMENT RT SIDE AT STA690 AIR DISTRIBUTION DUCT CRACKED. REPAIRED FWD CARGO COMPARTMENT RT SIDE AT STA690 AIR DISTRIBUTION DUCT BY REMOVING DAMAGE AND APPLYING FIBERGLASS FABRIC, IAW B757 AMM 21-23-01-8 REP NR 3 FIG 801.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 12. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681-RBL 18. REPLACED NUTPLATE AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV"F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE AT PRESSURE DECK THRU AFT PIT BULKHEAD PANEL BS 1681-RBL 36. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 "F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 39.5. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 32. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 24. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.
Part: STRUCTURE — DAMAGED (GALLEY DOOR TRIM) · airframe 76,969 hrs · 30,018 cycles
G1A GALLEY LOWER INBOARD DOOR TRIM DAMAGED AT LOWER INBOARD CORNER. ACCOMPLISHED FEDEX EA F-2530-T0358223-P1 EQUIP AND FURNISH-GALLEY-ICE CHEST DOOR TRIM-DAMAGED.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 4. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N 5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, LBL 24-BL 47. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071. MATERIAL LOSS .006. REMAINING MATERIAL THICKNESS .065 FOUND TO BE WITHIN LIMITS, IAW B757 SRM 53-60-51-1A TABLE 102. REPLACED NUTPLATE STRAP AS REQUIRED, IAW BOEING DRAWING 146N5693 REV "B" AND BOEING DRAWING 146N5300 REV "F" AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, BL 4-RBL 54. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071, MATERIAL LOSS .004 REMAINING MATERIAL THICKNESS .067 FOUND TO BE WITHIN LIMITS, IAW B757 SRM 53-60-51-1A TABLE 2. REPLACED NUTPLATE STRAP AS REQUIRED, IAW BOEING DWG 146N5693 REV "B" AND 146N5300 REV "F" AND B757 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 76,969 hrs · 30,018 cycles
MAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 24. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F" AND B757SRM 51-40-02.
Part: HYDRAULIC LINE — RUPTURED (LT MLG) · airframe 76,559 hrs · 29,708 cycles
LOSS OF ALL LEFT HYD FLUID. FOUND L MLG DOWN LOCK ACTUATOR LINE RUPTURED. R&R'D LINE IN REF TO AMM 32-32-02-4. RAN ENGINE AND ENGAGED EDP TO VERIFY PUMP INTEGRITY PER JRH. OPS CHECK GOOD, LEAK CHECK GOOD. OK FOR SERVICE
Part: SENSOR — INOPERATIVE (NLG) · airframe 76,434 hrs · 29,630 cycles
PDIS 780 32-30 4516 26FEB20 MEM OPEN U LOGPAGES:2877688 AFTER TAKEOFF, GEAR DISAGREE EICAS WITH AMBER GEAR LIGHT. GEAR EXTENDED NORMAL. NO EMERGENCY DECLARED. SHGN 26FEB20 22:32 MEM U DEBRIEFED FLIGHT CREW. DURING GEAR RETRACT RECEIVED GEAR DISAGREE WITH AMBER GEAR LIGHT. NO EICAS MESSAGES LATCHED IN FAULT REVIEW. PERFORMED PSEU FAULT REVIEW IAW FIM 32-09/802. ALL FAULTS LISTED ASSOCIATED WITH NLG. FAULT CODES: 238, 65, 66, 79, 78, 77. SHGN 27FEB20 09:32 MEM REMOVED AND INSTALLED NEW SYSTEM 2 NOSE GEAR LOCKED SWITCH REF. AMM 32-61-03-02. SPLICED WIRES FOR NEW SYS 2 NOSE GEAR LOCKED PROX SNSR SW AT SP28 AND SP30 REF WDM 31-61-22. REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT REF B757 AMM 32- 09-04-4. PERFORMED ADJ/TEST OF NOSE GEAR LOCK SWITCH IAW 757MM 32-61-03-2,NO FAULTS NOTED. PERFORMED NOSE GEAR EXTENSION /RETRACTION TEST IAW 757MM 32-34-00-5, NO FAULTS NOTED.
Part: SLIDE — DAMAGED (L1 DOOR) · airframe 76,421 hrs · 29,621 cycles
AFTER BLOCK IN FO DISARMED THE SLIDES AND CRACKED THE DOOR OPEN. WHEN GROUND CREW OPENED THE DOOR, THE SLIDE PARTIALLY DETAINED BUT DID NOT DEPLOY. INSTALLED L1 DOOR ESCAPE SLIDE ASSEMBLY IAW B757 25-66-01-4.
Part: CYLINDER — INOPERATIVE (L1 DOOR ASSIST) · airframe 76,421 hrs · 29,621 cycles
L1 DOOR EMERGENCY POWER RESERVOIR AT 0 PSI. REMOVED AND REPLACED LEFT #1 DOOR EMERGENCY POWER ASSIST RESERVOIR PER MM 52-11-30-4. PART REPLACED WAS A HR TEXTRON, ENTRANCE DOOR EMERGENCY POWER RESERVOIR, MPN 803300-35, MSN R21598. A/C OK FOR SERVICE.
2019
Part: STATIC LINE — OUT OF POSITION (R1 DOOR) · airframe 75,879 hrs · 29,255 cycles
UPON ARMING R1 WE DID NOT GET AN ARMED SLIDE LIGHT. F/O TRIED TO DISARM DOOR TO TRY AGAIN. DOOR WOULD NOT DISARM. IT APPEARS THE SLIDE WILL ARM BUT NO SLIDE ARMED LIGHT ILLUMINATES. FOUND SLIDE STATIC LINE WRAPPED AROUND GIRT BAR. REPOSITIONED STATIC LINE AS PER AMM 25-66-01-4 FIG 407. SLIDE ARMING AND INDICATION CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. NO PARTS CHANGED.
Part: COLLAR — WORN (L1 DOOR) · airframe 75,797 hrs · 29,205 cycles
L1 DOOR HOLD OPEN LOCK COLLAR BROKEN REMOVED AND REPLACED HOLD OPEN LOCK COLLAR ON L1 DOOR REF AMM 52-11-08-8. ALL DOOR CHECKS GOOD. PANEL REINSTALLED AND SEALED.
Part: LIGHT — MALFUNCTIONED (L1 DOOR ARMING) · airframe 75,632 hrs · 29,099 cycles
L1 DOOR SLIDE ARMED LIGHT NOT COMING ON AFTER ARMING DOOR PERFORMED OPERATIONAL CHECK ON SLIDE ARMED LIGHT IAW B757 AMM 25-66-11-2. OPS CHECK GOOD.
2018
Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,232 hrs · 28,832 cycles
LT OTBD FLAP UPPER SKIN INBD END SHOWS EVIDENCE OF POSSIBLE DELAMINATION. REPAIRED LT OTBD FLAP UPPER SKIN INBD END DELAMINATION IAW SRM 51-70-17-OG PARA 3G AND EA T F-5750-T0343415 P1 FLAP SKIN REPAIR.
2017
Part: PROXIMITY SENSOR — FAILED (GIRT BAR) · airframe 73,713 hrs · 27,827 cycles
SLIDE LIGHT FOR LT ENTRY DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED THE L1 DOOR GIRT BAR PROXIMITY SENSOR IAW MM 25-66-11-2 AND WDM 25-66-11, OPS CHECKED NORMAL.
2016
Part: SEAT TRACK — CORRODED (BS 345-377) · airframe 73,454 hrs · 27,635 cycles
MAIN CABIN SEAT TRACK BS 345 TO 377.70 LBL 6 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS .055 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52-1A. INSTALLED SEAT TRACK IAW SRM 51-40-02
Part: SEAT TRACK — CORRODED (BS 345-377) · airframe 73,454 hrs · 27,635 cycles
MAIN CABIN STA 345 TO 377.70 RBL 12 HAS CORROSION ON SEAT TRACK. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS .060 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52-1A. INSTALLED SEAT TRACK IAW SRM 51-40-02.
Part: FRAME — GOUGED (BS 231) · airframe 73,454 hrs · 27,635 cycles
BS 231 FRAME BUTLINE 0 IS GOUGED. REPAIRED IAW EA F-5310-T0329105 P1.
Part: COLLAR — CRACKED (L1 DOOR) · airframe 73,359 hrs · 27,562 cycles
L1 GUST LOCK FAILS TO LOCK THE DOOR IN OPEN POSITION. REPLACED THE DAMAGED HOLD/OPEN LOCK TRIGGER CATCH AND THE UPPER COLLAR.
Part: SKIN — DAMAGED (TE FLAP) · airframe 73,027 hrs · 27,322 cycles
REF WRI 05-50 1554 LT INBD MAIN & AFT FLAP HAS MULTIPLE HAIL DAMAGE DENTS. COMPLIED WITH EA F-5750-T0324301. LT WING INBD MAIN FLAP HAIL DAMAGE REPAIR.
Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 73,027 hrs · 27,322 cycles
RGHT HORIZONTAL PANEL, BETWEEN AUXILIARY & FWD SPAR, APPROX 40 DENTS CAUSED BY HAIL DAMAGE. COMPLIED WITH EA F-5510-TO324254. CAT B REPAIR, MAJOR REPAIR.
Part: SKIN — DAMAGED (TE FLAP) · airframe 73,027 hrs · 27,322 cycles
RIGHT INBD MAIN & AFT FLAP HAS MULTIPLE HAIL DAMAGE DENTS. COMPLIED WITH EA F-5750-T0324304. RT WING INBD MAIN FLAP HAIL DAMAGE REPAIR.
Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 73,027 hrs · 27,322 cycles
LEFT HORIZONTAL STAB, BETWEEN AUXILIARY SPAR & RUNT SPAR HAS 30 EA. DENTS, HAIL DAMAGE. COMPLIED WITH EA. F-5510-TO324253. HORIZONTAL STABILIZER, LET HORIZONTAL STAB HAIL DAMAGE UPPER SURFACE. CAT B REPAIR, MAJOR REPAIR.
Part: SPOILER — DENTED (LT WING) · airframe 73,027 hrs · 27,322 cycles
LEFT WING NR 12 SPOILER, HAS A DENT & HAIL. REMOVED & REINSTALLED NR 12 SPOILER IAW AMM 27-61-01-4. REPAIRED NR 12 SPOILER IAW SRM-51-70-03-5N. RESTORED FINISH IAW AMM 51-23-10-00. OPERATIONS CHECKED GOOD IAW-AMM-27-61-01-4, TR 14773 & TR 83336. REPAIR CAT A MAJOR REPAIR.
Part: SKIN — DAMAGED (LT SPOILER) · airframe 73,027 hrs · 27,322 cycles
LEFT WING NR 5 SPOILER, PUNCTURE ON UPPER SIDE, HAIL DAMAGE. REMOVED & REINSTALLED NR 5 SPOILER IAW-AMM-27-61-01-4. REPAIRED SPOILER IAW SRM-51-70-03-5N. RESTORED FINISH IAW AMM 51-23-10-00. ACCOMPLISHED OPERATIONS CHECK IAW AMM 27-6-01-4. OPERATIONS CHECKED GOOD, TR 14777, TR 85415. CAT A MAJOR REPAIR.
Part: SKIN — DELAMINATED (RT AILERON) · airframe 73,027 hrs · 27,322 cycles
RIGHT AILERON, WING STATION 681.1, DENT WITH DELAMINATION, HAIL DAMAGE. REPAIRED RT WING AILERON IAW SRM 57-70-17, RECALCULATED RT WING AILERON BALANCE MOMENT IAW SRM 51-60-01. NEW BALANCE MOMENT IS -11.372. CAT A MAJOR REPAIR.
2015
Part: SEQUENCE VALVE — MALFUNCTIONED (NLG) · airframe 726 hrs · 27,036 cycles
ON TAKEOFF GEAR DISAGREE LIGHT CAME ON WITH CAUTION LIGHT. HANDLE WAS IN UP POSITION BUT COULD HEAR GEAR DOWN. RAN QRH, PUT GEAR DOWN GOT 3 GREEN & CAME BACK TO LAND. AIRSPEED NEVER GOT ABOVE 210 KIAS. WHEN GEAR DISAGREE LIGHT WAS ON, THERE WAS NOISE COMING FROM THE NOSE OF THE ACFT. R & R NOSE GEAR DOOR ACTUATED SEQUENCE VLV. JACKED ACFT SWUNG GEAR.
2014
Part: SKIN — GOUGED (FUSELAGE) · airframe 72,031 hrs · 26,601 cycles
STATION 1440 STRINGER 23R - 24R SKIN EDGE HAS GOUGE MARKS. SKIN EDGE GOUGE MARKS COMPLIED WITH EA F-5330-T0312777 PART 1. TITLE FUSELAGE PLATES & SKINS EXISTING TRIM OUT LOCATIONS ON FUSELAGE SKIN AT BS 1440 BETWEEN STRINGERS 23R & 25R. REPAIR CLASSIFIED AS MAJOR.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
AFT CARGO COMPARTMENT BS 1460 - 1479 STRINGER 29 RT TO 30 ANTENNA RETAINER DOUBLER CORROSION FOUND AFTER ACCESS IAW SNRM NOO186. CORRODED ANTENNA RETAINER DOUBLER, RADIUS FILLER, REPLACED WITH NEW FABRICATED RADIUS FILLER IAW DWG 140N2058 SHT 1 REV A & EA F-5310-T0312842 PART 1. TITLE FUSELAGE MAINFRAME EXISTING EXTERIOR SKIN REPAIR AT BS 1460. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,031 hrs · 26,601 cycles
FUSELAGE SKIN AT STATION 1440 STRINGER 24R - 25R EDGE HAS EXISTING BLEND OFF. EXISTING BLEND OFF COMPLIED WITH EA F-5330-T0312777 PART 1. TITLE FUSELAGE PLATES & SKINS EXISTING TRIM OUT LOCATIONS ON FUSELAGE SKIN AT BS 1440 BETWEEN STRINGERS 23R & 25R. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 72,031 hrs · 26,601 cycles
AIRCRAFT INSPECTION FLOORBEAM BS 310, RBL 42, UPPER CHORD OF FLOORBEAM, FOUR EACH FASTENER COUNTERSINKS ARE TOO DEEP. LOCK FASTENER HEADS PULLING THROUGH UPPER SURFACE OF CHORD. FLOORBEAM UPPER T CHORD AT STATION 310 REMOVED IAW SRM 51-40-02 REV 113. NEW T CHORD FABRICATED IAW DWG 1415810 SHT 23 REV G & EA F-5310-T0311851 PT 1. ALTERNATE FINISHING FOR STATION 310 FLOORBEAM UPPER CHORD. FABRICATION & INSTALLED IAW DWG 141N5180 SHT 26 REV D & SRM 51-40-02 REV 113. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
AGEING ACFT, ACFT INSPECTION FLOORBEAM BS 1640, LBL 10 TO RT FRAME UPPER CHORD, LOWER SURFACE OF FLOORBEAM HAS MANY AREAS OF CORROSION AROUND NUTPLATE HOLES, REF N01875. FLOORBEAM AT STATION 1640 LBL 70 TO RBL 70 WAS R & R WITH NEW FABRICATED FLOORBEAM IAW DWG 146N5136 SHT 1 REV & 146N5089 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — CHAFED (FUSELAGE) · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE EXTERIOR SKIN THERE ARE NICKS & SCRATCHES AT STATION 1825 - 1844, STRINGER 5L - 6L. REMOVED & TREATED IAW SRM 51-10-02 & 51-20-01 REV 113, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET II ALLOWABLE DAMAGE 1 REV 113. REPAIR CARRIED OUT IAW PART 1 OF EA F-5330-T0312884 TITLE FUSELAGE PLATES & SKINS REPAIR FOR OUT OF LIMITS BLEND OUT FUSELAGE SKIN AT STATION 1825 - 1862 BETWEEN STRINGER 5L & 6L. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT BEAM — CHAFED (NR 2 NACELLE) · airframe 72,031 hrs · 26,601 cycles
NUMBER 2 STRUT FAN COWL SUPPORT BEAM INBD RAIL FOUND CHAFE MARK AT NAC STATION 98.5. REPAIRED IAW EA F-5450-T0312965 PART 1 TITLE NACELLES & PYLON, PYLON STRUCTURE NR 2 STRUT. LT & RT FAN COWL SUPPORT BEAM RAIL GOUGE BLEND OUT, REPAIRED. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT BEAM — CHAFED (NR 2 NACELLE) · airframe 72,031 hrs · 26,601 cycles
NUMBER 2 STRUT FAN COWL SUPPORT BEAM OTBD RAIL FOUND CHAFE MARK AT NAC STATION 98. REPAIRED IAW EA F-5450-T0312965 PART 1 TITLE NACELLES & PYLON, PYLON STRUCTURES NR 2 STRUT LT & RT FAN COWL SUPPORT BEAM RAIL GOUGE BLEND OUT REPAIR. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — DENTED (BS 1595) · airframe 72,031 hrs · 26,601 cycles
FUSELAGE EXTERIOR SKIN BS 1595 AT STRINGER 17R DENTED. REPAIRED IAW EA F-5330-T0313250 PART 1. REPAIR CALSSIFIED AS MAJOR.
Part: SKIN — CHAFED (E/E DOOR) · airframe 72,031 hrs · 26,601 cycles
FWD E & E BAY DOOR EXTERNAL SKIN CHAFED. REPAIRED IAW EA F-5310-T0313047. REPAIR CLASSIFIED AS MAJOR
Part: SKIN — CORRODED (BS 1160-1680) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
AFTER REMOVAL OF AFT DRAIN MAST, FUSELAGE SKIN EXTERIOR SURFACE FOUND CORRODED BETWEEN STRINGER 25 & 26R BS 1660 & 1680. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113. REPAIRED IAW EA F-5330- T0312967 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (BS 1844-1862) · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE SKIN HAD NICKS & SCRATCHES AT BS 1844 - 1862 STRINGER 5 - 6L. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 113, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET II ALLOWABLE DAMAGE 1 REV 113. REPAIRED IAW EA F-5330-T0312884. REPAIR CLASSIFIED AS MAJOR.
Part: INTERCOSTAL — CORRODED (BS 590) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
FORWARD CARGO BAY BS 590 INTERCOSTAL CORRODED. REMOVED AND REPLACED IAW DWG 143N6603 SHT 1 REV B. REPAIR CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
DURING REMOVAL OF ANCHOR NUT FROM OUTER STRAP ON THE APU AIR INLET DOOR CUT OUT FOUND OUTER STRAP FOUND EXFOLIATION CORROSION AT BS 1825 STRINGERS 3 - 6R. FOUND OUT OF LIMITS IAW SRM 53-80-15 TABLE 101 ALLOWABLE DAMAGE 1 REV 112. STRAP REMOVED AND REPLACED IAW DWG 148N3138 SHT 1 REV C, AND DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — SCRATCHED (BS 1700-1720) · airframe 72,031 hrs · 26,601 cycles
SKIN HAS A SCRATCH AT BS 1700 - 1720 BETWEEN STRINGERS 5 - 6R. REPAIRED IAW SRM 53-00-1 FIG 201 REPAIR 16 REV 113. REPAIR CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1681 - 1705 LBL 5 - RBL 5 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (BS 1681-1700) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1681 - 1700 RBL 20 - 24 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1681 - 1700 RBL 38 - 52 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1700 - 1720 RBL 22 - 52 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: DECK PLATE — CHAFED (ZONE 200) · airframe 72,031 hrs · 26,601 cycles
BS 1718 RBL 12 DECK PLATE CUT OUT FOUND CHAFED AT THE EDGE. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: FITTING — DAMAGED (NR 2) · airframe 72,031 hrs · 26,601 cycles
NR 2 PYLON AFT ENGINE MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE. REPAIRED IAW EA F-5450-T0311678. REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CHAFED (BS 1470-1480) · airframe 72,031 hrs · 26,601 cycles
BS 1470 - 1480 RBL 45.5 SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 112. REWORKED AREA EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 DETAIL 1 FIG 101 REV 113. SEAT TRACK REMOVED AND TRIMMED IAW SRM 53-00-52 FIG 201 OPTION 1 REPAIR 1 REV 113. REPAIR STRAP, ANGLE AND SEAT TRACK FABRICATED IAW SRM 53-00-52 REPAIR 1 FIG 201 OPTION 1 REV 113 AND INSTALLED IAW SRM 53-00-52 FIG 201 OPTION 1 REPAIR 1 REV 113. REPAIR CLASSIFIED AS MAJOR.
Part: FITTING — DAMAGED (ZONE 400) · airframe 72,031 hrs · 26,601 cycles
PYLON NR 1 PYLON AFT ENG MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE.
Part: FITTING — DAMAGED (ENGINE MOUNT) · airframe 72,031 hrs · 26,601 cycles
NR 1 ENGINE AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG HOLES FOUND OVERSIZED AFTER BUSHING REMOVAL. REPAIRED IAW EA F-7120-T0312223.
Part: FITTING — DAMAGED (ENGINE MOUNT) · airframe 72,031 hrs · 26,601 cycles
NR 2 ENGINE AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG HOLES FOUND OVERSIZED AFTER BUSHING REMOVAL. REPAIRED IAW EA F-7120-T0312222. REPAIR CLASSIFIED AS MINOR.
Part: FRAME SPLICE — GOUGED (BS 1520) · airframe 72,031 hrs · 26,601 cycles
AFT CARGO BAY BS 1520 STRINGER 24R - 25R FRAME SPLICE GOUGED. FOUND OUT OF LIMITS. REMOVED AND REPLACED THE FRAME SPLICE IAW DWG 146N1017 SHT 2 REV. E, AND DWG 146N1042 SHT 01 REV. A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
AFT CARGO BS 1380 S17-18R FRAME FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10- 02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 ALLOWANLE DAMAGE 2 REV 113. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 113, DWG 146N8511 SHT 1 REV J. REPAIR CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (BS 1825) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT MIDDLE STRAP FOUND CORRODED AT BS 1825 STRINGERS 3 - 6R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-15 FIG 101 TABLE 101 ALLOWABLE DAMAGE 1 REV 113. REPAIRED IAW SRM 53-80-15 FIG 202 DETAIL II REPAIR 1 REV 113 REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT ANGLE — CORRODED (BS 1789) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORROSION AT BS 1789, STRINGER 3R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT ANGLE — CORRODED (BS 1790-1825) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED BETWEEN BS 1790 - 1825 STRINGER 3R. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 112. SUPPORT ANGLE REMOVED AND REPLACED IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT ANGLE — CORRODED (BS 1790-1825) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1790- 1825 STRINGER 6R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3152 SHT 1 REV AND DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT ANGLE — CORRODED (BS 1789) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1789, STRINGER 6R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3141 SHT 1 REV B AND DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: SUPPORT — DAMAGED (RT WING) · airframe 72,031 hrs · 26,601 cycles
AFTER CARRIAGE SUPPORT REMOVAL ON RT WING, OTBD TE MAIN FLAP FRONT SPAR HAS THREE HOLES FOUND ELONGATION AT NR 8 CARRIAGE FWD SUPPORT FITTING ATTACH AREA. REPAIRED IAW EA F-5750-T0312509. REPAIR CLASSIFIED AS MINOR.
Part: ANGLE — CORRODED (BS 700-740) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 700 - 740 L2 DOOR LOWER SILL ANGLE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 112 AND FOUN OUT OF LIMITS IAW SRM 53-30-15 FIG 101 ALLOWABLE DAMAGE 2 REV 113. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02 REV 113 AND DWG 143N8322 SHT 1 REV K. REPAIR CLASSIFIED AS MAJOR.
Part: ANGLE — CORRODED (BS 320-360) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 320 - 360 R1 DOOR LOWER SILL ANGLE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-20- 01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53- 10-15 FIG 101 ALLOWABLE DAMAGE 1 REV 113. SILL ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 113 AND DWG 141N8422 SHT 01 REV R. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
Part: STRAP — CORRODED (BS 1787) · airframe 72,031 hrs · 26,601 cycles
EMPENNAGE APU AIR INLET DOOR CUT OUT FWD STRAP HAS CORROSION AT BS 1787 STRINGER 3 - 6R. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV 112. AND SRM 51-40-02 REV 113 AND DWG148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — DAMAGED (BS 345) · airframe 72,031 hrs · 26,601 cycles
BS 345 RBL 23 - 60 FLOORBEAM UPPER TEE FOUND DAMAGED. FLOORBEAM TEE REPAIRED IAW SRM 53-00-51 REPAIR 8 REV 113 REPAIR CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 960 - 984 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 112. REWORKED AREA EVALUATED AND FOUND MATERIAL LOSS OF 0.021" OUT OF 10% LIMIT OF ORIGINAL THICKNESS OF 0.063" IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 FIG 101 REV 113 DETAIL III. FABRICATED IAW DWG 144N5140 SHT 3 REV D. CREASE BEAM REMOVED AND REPLACED IAW SRM 51-40-02 REV 113 AND BOEING DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
FLOORBEAM AT BS 1661 CORRODED. FLOORBEAM TEE REMOVED BETWEEN RBL 70 - LBL 70 IAW SRM 51-40-02 REV 113. NEW FLOORBEAM TEE FABRICATED IAW DWG 146N5110 SHT 3 REV B AND INSTALLED IAW DWG 146N5090 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (BS 580-600) · airframe 72,031 hrs · 26,601 cycles
FUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26 LT & 26 RT AT BS 580- 600. DAMAGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113 AND REPAIRED IAW EA F-5330-T0312729 PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: WEB — CHAFED (NR 2 PYLON) · airframe 72,031 hrs · 26,601 cycles
NUMBER 2 PYLON OTBD SIDE FAN COWL SUPPORT WEB AFT SIDE EXISTING REPAIR. THERE IS WEAR MARK IN THE DOUBLER. SUPPORT WEB REPAIRED IAW EA F-5450-T0312881 PART 1. TITLE NACELLES & PYLON, PYLON STRUCTURES, RE-ACCOMPLISH EXISTING REPAIR AT NR 2 PYLON OTBD SIDE, FAN COWL SUPPORT WEB RSC TRACKING. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
AS PER CUSTOMER REQUEST, TO REPLACE FLOORBEAM AT STATION 377 DUE TO CORROSION. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
CABIN STATION 377.7 LBL 45 - 60 FLOORBEAM UPPER FLANGE FOUND CORROSION AT UPPER & LOWER SURFACES. COMPLIED WITH EA F-5310-T0313248 PART 1. TITLE FUSELAGE MAINFRAME FLOORBEAM INSTALLATION STATION 377, LBL 64, ADDITIONAL FASTENER COMMON TO FLOORBEAM & FRAME STACK UP & SHORT FASTENER SPACING. REFER TO SNRM N03607 FOR WORK DETAILS.
Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1661 LBL 1 - 20 FLOORBEAM UPPER FLANGE FOUND CORRODED. REPAIRED IAW DWG 146N5110 SHT 3 REV B AND DWG 146N5090 SHT 6 REV . REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1661 RBL 15 - 26 FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW DWG 146N5110 SHT 3 REV B AND DWG 146N5090 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1681 FLOORBEAM UPPER FLANGE FOUND CORRODED AT RBL 20 - 24. CORROSION REMOVED IAW SNRM N02361. REPAIRED IAW EA F-5310-T0311890 A PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
FLOORBEAM AT BS 1681 CORRODED. REPLACED IAW EA F-5310-T0311890 A PART 1. REPAIR CLASSIFIED AS MAJOR.
Part: DOOR SILL — CORRODED (BS 1701-1720) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
BS 1701 - 1720 R4 DOOR CUT OUT LOWER SILL WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 113. LOWER SILL WEB FABRICATED IAW DWG 146N8723 SHT 05 REV -. FABRICATED LOWER SILL WEB INSTALLED IAW DWG 146N8722 SHT 03 REV B REPAIR CLASSIFIED AS MAJOR
Part: DOOR SILL — CRACKED (BS 333-377) · airframe 72,031 hrs · 26,601 cycles
BS 333 -377 L1 DOOR CUT OUT LOWER SILL WEB FOUND CRACK AT STATION 334 AFTER WEB. REPLACED WITH NEW FABRICATED WEB IAW DWG 141N8422 SHT 01 REV R. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 72,031 hrs · 26,601 cycles
RIGHT WING UPPER SKIN SURFACE FOUND CORRODED AT OVERWING FILL PORT ADAPTER MATING AREA. CORROSION REMOVED & AREA REPAIRED IAW EA F-5730-T0312814 P1. REPAIR CLASSIFIED AS MAJOR.
Part: SPAR — CHAFED (TE FLAP) · airframe 72,031 hrs · 26,601 cycles
RIGHT WING REFER TO SNRM N00617, AFTER CARRIAGE SUPPORT REMOVAL, OTBD TE. MAIN FLAP FRONT SPAR WEB FOUND CHAFE MARK AT NR 8 CARRIAGE FWD SUPPORT FITTING MATING AREA. REPAIRED IAW EA F-550-T0312509. REPAIR CLASSIFIED AS MINOR.
Part: FASTENER — LOOSE (FLAP TRACK) · airframe 72,031 hrs · 26,601 cycles
RIGHT WING OTBD TE MAIN FLAP OTBD CARRIAGE FWD MOUNT SUPPORT, FOUND ONE LOCK FASTENER BROKEN & TWO LOCK FASTENERS LOOSE. REPAIRED IAW EA F-5750-T0312509. REPAIR CLASSIFIED AS MINOR.