N959FD
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.
148 reports on file, 2012-03-05 – 2023-05-04.
Part: UNKNOWN — UNKNOWN (N/A) · airframe 54,979 hrs · 25,874 cycles
PDIS 959 21-30 9546 03MAY23 IND OPEN U AT FL 350 WE RECEIVED A CABIN ALT MASTER WARNING AND EICAS WARNING. CABIN ALT WAS AT 10,000 FT. COMPLIED WITH QRH. CABIN ALT CLIMBED TO 11,000 FT BEFORE WE WERE ABLE TO DESCEND. AROUND FL 180 CABIN ALT LIGHT WENT OUT. ***EMERGENCY DECLARED*** 1 SHGN 03MAY23 22:17 IND U NRR: NO REFERENCE REQUIRED AFTER ACFT BLOCKED IN OPENED BOTH PACK BAYS AND FOUND BOTH PACK DISCHARGE DUCTS ORANGE BOOTS DISLODGED FROM DUCTING. PART 03MAY23 22:23 IND U IDENTIFIED PARTS HOSE MPN: AS1505-28A0032 CPN: 2113640 QTY: 2 PART 03MAY23 22:23 IND U ORDER PART MPN: AS1505-28A0032 CPN: 2113640 QTY: 2 MSN: 2147651 AMM: 21-51-00 REMOVED AND REPLACE R/H PACK BAY AND L/H PACK BAY ORANGE PACK SUPPLY BOOTS REF 757 AMM 21-51-00 AND 21-51-10-4. OPS AND LEAKS CHECKS GOOD REF 21-31-00-5. A/C OK FOR SERVICE. AS AN SDR ITEM, PARTS WERE A TL 0 - BOTH LH AND RH SUPPLY BOOT P/N'S WERE AS1550-28A0032 (HOSE) , CPN 2113640
Earlier reports · 2012–2022 · 147 reports
2022
Part: ENGINE — LEAKING (RIGHT) · airframe 54,397 hrs · 25,489 cycles
PDIS 959 73-20 8902 23JUN22 JAX OPEN U LOGPAGES:386108 ON TAKEOFF, CLIMB, RIGHT ENGINE DID NOT REACH TAKEOFF POWER SETTING. OM CLIMB OUT RIGHT ENGINESURGING WHEN SELECTED VNAV TMSP DID NOT GO INTO CLIMB MODE AND PROGRAMMED SPEEDS IN FMS DID NOT MAKE ITS TRANSITION TO CLIMB SPEEDS 200 TO 250. SHGN 23JUN22 02:04 JAX U PER CREW DEBRIEF: DURING TAKEOFF WITH AUTO THROTTLES ENGAGED (TARGET TAKEOFF EPR WAS 1.56) RIGHT ENGINE ONLY ACHIEVED 1.43-1.48 INDICATED EPR. ON CLIMB TURNED OFF AUTO THROTTLES, BUT SURGING DIDNT STOP UNTIL POWER WAS REDUCED AND EEC(S) SELECTED OFF (PER QRH). STATED WITH AUTO THROTTLES ON RIGHT ENGINE WAS "TRYING TO OVERTEMP (BUT DID NOT) TO ACHIEVE MATCHED TAKEOFF EPR". CREW TOOK PIC OF CRUISE ENGINE INDICATIONS (MATCHING ALL BUT EPR) FROM PREVIOUS FLIGHT GSO TO JAX, AUTO THROTTLES WERE OFF, EEC(S) WERE OFF. INDICATING THAT THE RIGHT ENGINE EPR WAS ONLY INDICATION THAT WAS UNMATCHED. 1.43 EPR 1.25 82.1% N1 82.3% 580' EGT 558' 80% N2 80% 83% N3 83% 3.6 FF 3.5 GAINED ACCESS AND INSPECTED PF RAKES, ALL PITOT HEADS CLEAN AND INTACT. NO DEBRIS FOUND. PRESSURIZED PF AIR LINE FROM EPR TRANSMITTER AND FOUND LEAK AT HARD LINE CAP ON FIREWALL, JUST BEHIND FFG. REMOVED CAP, CLEANED THREADS FACT 23JUN22 22:51 JAX PERFORMED MPA PER 71-00-00-5-3 TARGET EPR OF 1.68 WAS REACHED WITH EEC ON AND OFF. ACFT OK FOR SERVICE
Part: SKIN — GOUGED (RT WING FLAP) · airframe 54,396 hrs · 25,487 cycles
RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL GOUGED REPAIRED RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL IAW B757 SRM 57-53-01-2R-1 AND 51-70-10-2R REPAIR 4
Part: WEDGE — DELAMINATED (RT WING FLAP) · airframe 54,396 hrs · 25,487 cycles
R/W I/B FWD FLAP LOWER SURFACE T/E WEDGE IS DELAMINATED REMOVED AND REPLACED WEDGE PER BOEING DWG # 113N2603
Part: DOUBLER — CRACKED (NR 2 NACELLE) · airframe 54,396 hrs · 25,487 cycles
#2 ENGINE PYLON INTERNAL SPLICE STRAP FOR PANELS 441AL AND 442AL RUBSTRIP IS CRACKED AND BROKEN IN SEVERAL SPOTS. REMOVE REPAIRED AND REINSTALLED PER BAC DWG 313N5003 REV Y AND FEDEX EA F-5450-T0368926 TITLE: NACELLES/PYLONS - WING PYLON/STRUT - NO 2 PYLON UPPER FAIRING - PPSTA 103 - INTERNAL SPLICE STRAP DOUBLER - ALTERNATE SURFACE.
Part: FAIRING — CRACKED (NR 1 NACELLE) · airframe 54,396 hrs · 25,487 cycles
#1 PYLON AFT NACELLE TRAILING EDGE IS CRACKED FWD OF THE SAIL BOAT FAIRING. REPAIRED FAIRING SKIN PER FEDEX EA # F-5480-T0368778 TITLE: NACELLES/PYLON - FILLETS/FAIRINGS - LH STRUT AFT FAIRING, TRAILING EDGE SKIN, CRACK REPAIR.
Part: SKIN — CRACKED (LT WING SLAT) · airframe 54,396 hrs · 25,487 cycles
L/W #3 SLAT I/B TRACK COVE PANEL IS CRACKED ON I/B SIDE REMOVED AND REPLACED PER BOEING DWG # 114N4077 REV F
Part: COVER — CRACKED (NR 1 ENGINE) · airframe 54,396 hrs · 25,487 cycles
#1 ENGINE I/B FAN COWL UPPER AFT HINGE COVER IS CRACKED. REPAIRED HINGE COVER PER FEDEX EA F-7110-T0368874 TITLE: POWERPLANT - WING ENG COWL - NO 1 INBD FAN COWL, HINGE SHIELD, CRACK AND DENT DAMAGE.
Part: STRIP — CRACKED (NR 1 NACELLE) · airframe 54,396 hrs · 25,487 cycles
#1 PYLON FWD CHAFE STRIP UNDER PANEL 431AL IS WORN , CRACKED AND MISSING. REMOVED AND REPLACED CHAFE STRIP PER BAC DWG 313N5036 REV M, BAC 5000 AND B757 SRM 51-40- 02
Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 54,396 hrs · 25,487 cycles
RIGHT MAIN LANDING GEAR WHEEL WELL WING TO BODY SUPPORT ANGLE IS CRACKED APPROX. BS1088 REMOVED, FABRICATED NEW PART, AND INSTALLED PER BAC DWG 149N7552 REV F
Part: WEB — DAMAGED (CARGO DOOR) · airframe 54,396 hrs · 25,487 cycles
MCD LOWER INTERNAL WEB IS DAMAGED IN 2EA LOCATIONS AT APPROX STA 580 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
Part: WEB — DAMAGED (CARGO DOOR) · airframe 54,396 hrs · 25,487 cycles
MCD LOWER INTERNAL WEB IS DAMAGED IN 2EA LOCATIONS AT APPROX STA 500 AND STA 520 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
Part: STOP FITTING — GOUGED (L1 DOOR) · airframe 54,396 hrs · 25,487 cycles
L1 DOOR UPPER FWD DOOR STOP IS GOUGED REMOVED, LOCATED, DRILLED AND INSTALLED NEW STOP FITTING IAW B757-2 DWG 141N8371 REV J AND 141N8341 REV D
Part: GUST LOCK — BROKEN (N/A) · airframe 54,292 hrs · 25,430 cycles
L1 DOOR GUST LOCK BROKEN PERFORMED ADJUSTMENT/ TEST ON L1 DOOR REF AMM 52-11-00-5. NO DEFECTS NOTED. OKAY FOR SERVICE
2021
Part: TRANSMISSION — LOW QUANTITY (LT WING TE FLAP) · airframe 53,726 hrs · 25,055 cycles
WHEN SELECTING FLAPS TO 20, GOT TE FLAPS DISAGREE EICAS. COMPLIED WITH QRH, TRAILING EDGE LIGHT DISAPPEARED. LANDED WITHOUT ISSUE. FOUND LEFT WING OB FLAP TRANSMISSION FOR IB FLAP VERY LOW ON FLUID. SERVICED WITH BRACO 795 PER B757 AMM 12-13-06-3. RAN FLAPS THROUGH SEVERAL CYCLES WITH NO FAULTS. A/C OK FOR SERVICE.
2020
Part: SENSOR — INOPERATIVE (EMERGENCY EXIT) · airframe 52,694 hrs · 24,417 cycles
PDIS 959 52-70 7383 30SEP20 MEM OPEN U. RT EMERGENCY DOOR EICAS MESSAGE DURING CRUISE. PRESSURIZATION APPEARED NORMAL. SHGN 30SEP20 09:25 MEM U SHGN 30SEP20 09:25 MEM U. FOUND GAP BETWEEN TARGET AND SENSOR AT NUMBER 3 RT EMERGENCY EXIT DOOR TO BE TOO SMALL. REMOVED SHIM MATERIAL TO GET GAP TO 0.14", IAW B757 AMM 52-71-00-5. STILL NEED TEST TASK 52-71-00-735-053. PART 30SEP20 10:09 MEM U. IDENTIFIED PARTS NOSE GEAR UP SENSOR MPN: 284N1641-5 CPN: 3217188 QTY: 2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 680 - 700 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 680 TO STA 700 LBL 60 ORIGINAL MAT .050", MATERIAL LOSS .010", MAT REMAINING .040" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02-OG AND B. DWG 143N5410 REV F.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 740 - 720 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 720 TO STA 740 LBL 60 ORIGINAL MAT .050" 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02-OG AND DWG 143N5410 REV F.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 700 - 720 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 700 - 720 LBL 63. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-OG AND B DWG 143N5410 REV F. ORIG MAT 0.056", MAT REMOVED 0.0008", MAT REMAINING 0.048" OUT OF LIMITS IAW SRM 51-10-02-OG & 53-00-51-1A DETAIL III.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 700 - 720 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 700 - 720 LBL 63. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-OG AND B DWG 143N5410 REV F. ORIG MAT 0.050", MAT REMOVED 0.010", MAT REMAINING 0.040" OUT AT LIMITS IAW SRM 51-10-02-OG & 53-00-51-1A DETAIL III.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 680 - 700 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 680 TO STA 700 LBL 63 ORIGINAL MAT .056", MAT LOSS .017" , REMAINING .039", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02-OG AND B DWG 143N5522 REV-.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN CABIN FLOOR SUPPORT STA 740-720 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 720 TO STA 740 LBL 63 ORIGINAL MAT .056" 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02-OG AND DWG 143N5522 REV-.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN DECK BETWEEN STA 1180-1200 RBL44.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT SEAT TRACK FLANGE STA 1180 - 1280 RBL 44.5, ORIG MAT 0.090", MAT REMOVED 0.060", MAT REMAINING 0.030", OUT OF LIMITS IAW SRM 53-00-02-1A. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-40-05-OG AND 51-40-02-OG & DWG 146N5120 REVA.
Part: SEAT TRACK — CORRODED (BS 1060) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN DECK BS 1060, LBL 58 SEAT TRACK FLANGE CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. ORIG MAT .070 REM .046 LOSS .024, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW IAW SRM 53-40-52-01, 51-40-05, 51-40-58, AND DWG 657N3332, REV A.
Part: FLOORBEAM — CRACKED (BS 1018) · airframe 52,470 hrs · 24,281 cycles
MAIN DECK BS 1018 BETWEEN RBL 24.75 - RBL 44.5 FLOOR SUPPORT DAMAGED. REMOVED COVER PLATE CRACKED AT BS 1018 BETWEEN RBL 24.75 - RBL 44.5. FABRICATED AND INSTALLED NEW COVER PLATE IAW DWG 144N5081 REV. A,C, AND SRM 51-40-02-OG.
Part: FLOORBEAM — CRACKED (BS 1055) · airframe 52,470 hrs · 24,281 cycles
MAIN DECK STA 1055 BETWEEN LBL 24.75 - LBL 44.5 FLOOR SUPPORT CRACKED. REMOVED COVER PLATE CRACKED AT STA 1055 BETWEEN LBL 24.75 - LBL 44.5. FABRICATED AND INSTALLED NEW COVER PLATE IAW DWG 144N5081 REV. A,C AND SRM 51-40-02-OG.
Part: PLATE — CORRODED (BS 1017) · corrosion level 2 · airframe 52,470 hrs · 24,281 cycles
MAIN DECK STA 1017 BETWEEN LBL 24.75 FLOOR SUPPORT CORRODED. MAIN DECK STATION 1017 BETWEEN LBL 24.75 - 44.50 FLOOR SUPPORT PLATE 100% MATL. LOSS REMOVED PLATE,FABRICATED AND INSTALLED NEW PLATE IAW BOEING DWG 144N5081 REV C/A. AND B 757 SRM 51-40-02-OG.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,415 hrs · 24,256 cycles
EMERGENCY EXIT SIGN OVER R1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSY (POWER SUPPLY) M730 REF AMM 33-51-07-2. REMOVED AND REPLACED R1 EMERGENCY EXIT SIGN REF AMM 33-51-01-2. EMERGENCY LIGHTS OPS CHECK GOOD.
Part: GUST LOCK — DAMAGED (ENTRY DOOR) · airframe 52,192 hrs · 24,110 cycles
DURING SERVICE FOUND LT ENTRY DOOR GUST DOOR LOCK BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN GUST LOCK REF AMM 52-11-08-8. MATERIAL 140N6008-1 COLLAR ASSY MATERIAL 140N6009-1 CATCH ASSY.
2019
Part: COVER — DISLODGED (LIFE RAFT) · airframe 51,920 hrs · 23,950 cycles
GROUND PERSONNEL DISLODGED COVER FOR RAFT AT L1. CALLED MX TO RESEAT INSTALLED L1 DOOR SLIDE COVER REF. 757 AMM 52-11-02-4. A/C OK FOR SERVICE.
Part: WIRE — BROKEN (HEATER) · airframe 51,035 hrs · 23,427 cycles
DURING CRUISE F/O TURNMED ON FOOT HEATER AND A SPARK AND A POP WAS FOLLOWED BY ELECTRICAL SMOKE. TURNED HEATER OFF AND SMOKE DISSIPATED. FOUND WIRES TO F/O LEFT FOOT HEATER BROKEN. REPAIRED BROKEN WIRES PER SWP CHAPTER 20-30 REFERENCING WIRING DIAGRAM 21-45-11. ALSO REMOVED AND REPLACED F/O LEFT FOOT HEATER PER MM 21-45. OPS CKS GOOD. A/C OK FOR SERVICE.
2018
Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 50,746 hrs · 23,259 cycles
RIGHT SIDE EMERGENCY SLIDE LIGHT INOP. RELAMPED RT EMERGENCY EVACUATION SLIDE LIGHT AS PER AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,396 hrs · 23,051 cycles
MAIN CABIN FLOORBEAM, CRACK IN UPPER SURFACE AT FS 324 AND APPROX RBL 55. REMOVED CORROSION IAW SRM 51-10-02-0G, EVALUATED AREA ORIGINAL MAT .120", MAT REMAINING .077", MAT LOSS .043", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG DETAIL VI, CUT OUT, FABRICATED AND INSTALLED REPAIR FLOORBEAM SECTION STA 324, RBL 12.5 TO RBL 70 IAW SRM 53-10-08-2R FIG 201 DETAIL II REPAIR 1. (NOTE: NO CRACK FOUND.)
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,396 hrs · 23,051 cycles
MAIN CABIN, COURIER SEAT TRACK, CORROSION ON UPPER SURFACE AT RBL 12 AND BETWEEN FS 345 AND FS 365. REMOVED CORROSION ON SEAT TRACK AT CABIN COURIER AREA FS 345 TO 365 RBL 12 AND EVALUATED DAMAGE ORIG. MAT: .070", MAT LOSS: .011", MAT. REM: .059" FOUND OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 DET VII. LOCATED AND DRILLED AND TRIMMED NEW SEAT TRACK SECTION IAW SRM 51-40-05-0G AND VA DWG 3470 REV G AND VA DCN 3504-NC-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-40-02-0G AND VA DWG 3470 REV G.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,396 hrs · 23,051 cycles
MAIN CABIN FLOOR SUPPORT CORROSION ON UPPER SURFACE BETWEEN FS 345 AND FS 365 AT BL 0. REMOVED CORROSION ON FLOOR SUPPORT ORIGINAL MAT .063", MAT REMAINING .020". MAT LOSS .043", FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G AND 53-00-51-1A DETAIL III FIG 101, REMOVED, LOCATED, DRILLED, TRIMMED AND INSTALLED NEW FLOOR SUPPORT SECTION IAW SRM 51-40-02-0G, B DWG 141N5111 REV C AND 657N3351 REV -.
Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 50,195 hrs · 22,932 cycles
DURING APPROACH TO LANDING TE FLAP DISAGREE APPEARED ON EICAS. FLAPS WOULD NOT MOVE, STUCK ABOUT 22. EXECUTED MISSED APPROACH AND FOLLOWED QRH. UNEVENTFUL LANDING AFTER DECLARING EMERGENCY. PERFORMED BITE TO FSEU NR 1, NR 2, & NR 3 AND CYCLED SEVERAL TIMES FLAPS/SLATS, IAW FIM 27-51-00 FIG107. NO CURRENT FAULTS FOUND. OK FOR SERVICE.
2017
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,499 hrs · 22,524 cycles
R1 DOOR EMERGENCY SLIDE LIGHT FOUND INOPERATIVE DURING TEST. REPLACED THE LAMP AND OPS CHECKED NORMAL IAW MM 33-51-06-2-1. ACFT OK FOR SERVICE.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,814 hrs · 22,091 cycles
RT FWD EMERGENCY SLIDE EVACUATION LIGHT INOP. PERFORMED EMERGENCY LIGHTS OPS CHECK IAW AMM.
Part: CABLE — OUT OF RIG (L1 DOOR) · airframe 48,385 hrs · 21,784 cycles
L1 DOOR FAILED DISARM CABLE CHECK. DIMENSIONS REQUIRED 1.6 INCHES, ACTUAL MEASUREMENT IS 1.3 INCHES. UNABLE TO ADJUST CABLE TO LIMITS. PERFORMED RIG ON DISARM CABLE. ALL ADJUSTMENTS & MEASUREMENTS ARE WITHIN LIMITS. ALL DOOR FUNCTIONS OPERATE NORMAL.
2015
Part: ROLLER — FAILED (L1 DOOR) · airframe 475 hrs · 21,315 cycles
ON TAXI OUT, LT FWD ENTRY DOOR LIGHT ILLUMINATED. INSTALLED A NEW UPPER LATCH CAM ROLLER. PERFORMED ADJUSTMENT TEST IAW MM 52-11-00-5. DOOR OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: HANDLE — DETACHED (COCKPIT) · airframe 471 hrs · 21,087 cycles
PARKING BRAKE HANDLE CAME OFF WHEN SETTING BRAKES AFTER PUSH BACK. R & R PARKING BRAKE LEVER IAW AMM 32-44-01-4. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
2014
Part: BATTERY — DISCHARGED (CABIN) · airframe 46,969 hrs · 20,952 cycles
RIGHT SIDE EMER EXIT SIGN STAYS ON 20 SECS & THEN GOES OUT DURING TEST, LT SIDE NORMAL. R & R RT EMER EXIT POWER SUPPLY BATTERY & PERFORM OPERATIONAL TEST IAW AMM 33-51-07-2 & 33-51-00-5. LIGHTS CHECKED NORMAL, OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,818 hrs · 20,867 cycles
R1 OUTSIDE EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW AMM. OPERATIONS CHECKED NORMAL.
2013
Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,901 hrs · 20,244 cycles
DURING CRUISE, CLIMBED FROM FL 370 TO FL 390 IN AREA OF HEAVY STATIC ELEC AND ST ELMO`S FIRE BOTH PILOTS SMELLED STRONG ODOR, LIKE BURNED RUBBER. ODOR DISSIPATED WITHIN FIVE MINUTES. ON DESCENT, PASSING 15000FT ODOR RETURNED. DONNED 02 MASKS, RAN "SMOKE FIRE OR FUMES" CHECKLIST. ODOR AGAIN DISSIPATED IN ABOUT FIVE MINUTES. NO OTHER ABNORMAL INDICATIONS, NO SMOKE SEEN. COMPLETED APPLICABLE ENGINE RUNS AT MAX STATIC EPR IAW CHAPTER 7 AND COMPLETED ALL STEPS IAW FIM 21-00-01. OPS TEST SATISFACTORY. NO ABNORMAL ODORS. NOTICED DURING ANY TEST OR ENGINE RUN. OK TO CONTINUE.
2012
Part: GIRT BAR — DIRTY (L1 DOOR SLIDE) · airframe 45,441 hrs · 19,914 cycles
L1 DOOR SLIDE ARMED KNOB IS NOT FUCTIONING CORRECTLY. REMOVED DEBRIS FROM FLOOR GIRT BAR ATTACHMENTS IAW MM RF 25-66-10-2. PERFORMED INSPECTION CHECK IAW MM REF. 52-11-00-6. OK FOR SERVICE. FINAL CLOSED.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,381 hrs · 19,880 cycles
EXTERIOR EVACUATION SLIDE LIGHT FOR R1 DOOR INOP WHEN TESTED. R & R ESCAPE SLIDE EMERGENCY LIGHT BULB, OPS CHECK NORMAL, REF AMM 33-51-06-2-1 OK FOR SERVICE.
Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT) · airframe 45,186 hrs · 19,743 cycles
EMERGENCY LIGHT INOPERATIVE. CLEANED RECEPTACLE AND RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD, ACFT OK FOR SERVICE.
Part: SKIN — DENTED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN DENTED AT BS 680-700 BETWEEN S25-26 RT. REPAIRED IAW EA F-5330-161080, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 100) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN DAMAGED AT BS 1440-1460 BETWEEN STR 19-20 RT. REPAIR CARRIED OUT ON BLENDED SKIN AT BS 1440-1460, STR 19R-20R, IAW EA F-5310-155896 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (R1 DOOR) · airframe 45,137 hrs · 19,707 cycles
CABIN, DURING REPLACEMENT OF DOOR R1 LOWER TORQUE TUBE BEARING, NOTICED TOOLING MARK IN DOOR SKIN AT AFT LOWER. REPAIRED IAW EA F-5210-155898, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
CABIN DURING REPLACEMENT OF FLOORBEAM FOUND CORROSION ON UNDERSIDE OF CREASE BEAM WEB AT BS 377 TO 395 LT. R & R WITH CREASEBEAM, FABRICATED IAW DWG 141N8322 SHEET 1, REV K AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 141N8322 SHT 1, REV K. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (BS 1825) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
AFTER REMOVAL OF THE STRAP AT BS 1825 FROM STRINGER 4 - 7 R FOUND OUTER STRAP HAS CORROSION. R & R WITH STRAP FABRICATED IAW DWG 148N3138, SHT 1, REV C AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
CREASE BEAM CORRODED AT BS 755 - 760. REPAIRED IAW EA F-5310-158189, PART 1. REPAIR IS CLASSIFIED AS MINOR.
Part: SHIM — MIGRATED (ZONE 500) · airframe 45,137 hrs · 19,707 cycles
LT WING BETWEEN OTBD NACELLE FITTING AND LOWER WING SKIN, FOUND SHIMS MIGRATING AT LWS 303.5. SHIMS TRIMMED IAW EA F-5740-158167, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SILL — CORRODED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
WHILE REMOVING CORROSION ON R2 DOOR LOWER SILL AREA, FOUND CORROSION SPREAD TO DOOR LOWER SILL INNER CHORD AT BS 670-730. R & R IAW SRM 51-40-02, REV 105 AND DWG 143N8322 SHT 1, REV K. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
CREASE BEAM RT SIDE IS CORRODED ON THE BOTTOM SIDE AT BS 365-377. R & R WITH CREASEBEAM FABRICATED IAW DWG 141N8422, SHT 1, REV R AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 141N8422 SHT 1, REV R. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 418 - 440 RBL 48 HAS CORROSION. FABRICATED IAW DWG 141N5131, SHT 3, REV C AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 141N5130, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — WORN (ZONE 300) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN FOUND ADDITION WORN BELOW THE HORIZONTAL STABILIZER CUTOUT AT BS 1850 - 1862 RT. R & R IAW DWG 148N7307 SHEET 1, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
AFTER REMOVAL OF FWD CARGO LOWER RT SIDE PANEL FOUND 1 FASTENER HOLE CLOSE TO NEXT FASTENER HOLE AT BS 740, STR 25 - 26R. REPAIR CARRIED OUT IAW EA F-5310-158170, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — NICKED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN AT BS 1600 -1620, S26L - 26R HAS NUMBEROUS NICKS IN SKIN. REPAIRED IAW SRM 53- 00-01 FIG 201, REPAIR 15, REV 106. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME SPLICE — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
AFTER REMOVAL OF FWD CARGO LOWER COMPT FLOOR RT SIDE PANEL, FOUND FRAME SPLICE ANGLE 1 FASTENER HOLE WITH SHORT EDGE MARGIN AT S 740 BETWEEN STR 25 - 26R. R & R IAW EA F-5310-158170, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
APU INLET AREA AT BS 1825 BETWEEN STR 4 - 7 RT THE NUTPLATE ATTACH STRAP IS CORRODED. CORRODED NUTPLATE ATTACHMENT STRAP REMOVED. NUTPLATE STRAP FABRICATED IAW DWG 148N3138 SHT 1, REV C AND INSTALLED IAW DWG 148N3105 SHT 1. REV C. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
BS 1688 TO 1694, LBL 15 TO LBL 16 HAS CORROSION. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
DECK PLATE HAS CORROSION AT BS 1681 TO 1684 AT LBL 6. REPLACED WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV.105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — GOUGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
BS 1685 TO 1694 LBL 54 GOUGED IN DECK PLATE. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02 REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REVA. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
CABIN DECK PLATE HAS CORROSION AT STA 1690 TO STA 1717 BL 0. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV 105 AND DWG 146N5300. SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CORROSION ON DECK PLATE AT BS 1683 TO 1687, RBL 51. REPLACED WITH FABRICATED DECK PLATE IAW SRM 51-40-02 REV.105 AND DWG 146N5300 SHT.1 REV.E AND SHT.3 REV.A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
DECK PLATE HAS CORROSION AT BS 1716, LBL 54 TO RBL 54. REMOVED AND REPLACED WITH DECK PLATE FABRICATED AS PER DWG 146N5310 SHT.3 REV. AND INSTALLED IAW SRM 51-40-2 REV. 105 AND DWG 146N5300 SHT 1, REV E, AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
CABIN DECK PLATE AT BS 1707 TO 1713, RBL 15 CORRODED. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
DECK PLATE AT BS 1681, RBL 34 TO RBL 45 HAS CORROSION INSIDE FASTENER HOLES. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
EMPENNAGE RT SIDE THE APU INLET FWD EDGE NUTPLATE STRAP HAS CORROSION AT BS 1790 BETWEEN STR 4 - 7 RT. R & R IAW DWG 148N3105, SHT 1 REV C. REPAIR IS CLASSIFIED AS MAJOR.
Part: SILL — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
AFT CARGO BAY DOOR CUTOUT AREA LOWER SILL NEAR BS 1414 LOWER SECTION DAMAGED. REPAIRED IAW EA F-5310-158036. REPAIR IS CLASSIFIED AS MINOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
CABIN, FOUND CORROSION ON DECK PLATE AT STA 1682 RBL 3. REPLACED WITH FABRICATED DECK PLATE IAW SRM 51-40-02 REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
DECK PLATE AT BS 1690 TO 1696 RBL 15 CORRODED. R & R WITH FABRICATED DECK PLATE IAW SRM 51-40-02, REV 105 AND DWG 146N5300 SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: ATTACH ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
EMPENNAGE, APU INLET MOUNTING AREA AT BS 1790 - 1823 STR 7R THE NUTPLATE ATTACH ANGLE CORRODED. REMOVED, & FABRICATED IAW DWG 148N3152 SHT1, REV - INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: ATTACH ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
EMPENNAGE, APU INLET AREA AT BS 1790 - 1823 STR 4 R THE NUTPLATE ATTACH ANGLE CORRODED. R & R WITH NUTPLATE ANGLE FABRICATED IAW DWG 148N3152, SHT 1 REV AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
CABIN DECK PLATE HAS CORROSION AT STA 1680 TO 1717 RBL 35. REPLACED IAW SRM 51-40-02 REV 105 AND DWG 146N5300, SHT 1, REV E AND SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 45,137 hrs · 19,707 cycles
NR 1 NACELLE STRUT PYLON STRUCTURE INBD ACCESS HOLE CUT-OUT INNER EDGES FOR PANEL NR 433LR FOUND WITH 1" CRACK AT PPSTA 185.0. AREA TRIMMED AND REPAIR CARRIED OUT IAW EA F-5450-158034, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FLOORBEAM AT BS 1280, LBL 35 CORRODED. R & R WITH FLOORBEAM FABRICATED DWG 146N5044 SHT 1, REV A AND INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 146N5005 SHT 1, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FLOORBEAM AT BS 128, LBL 27 CORRODED. R & R WITH FABRICATED FLOORBEAM IAW SRM 51-40-02. REV 105 AND DWG 146N5005, SHT 1, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
AFT LOWER CARGO BAY FRAME, BS 1540 STRINGER 26L UPPER FLANGE DENTED. REPAIRED IAW SRM 53-00-07, FIG.201, DETAIL I, REPAIR 5, REV 106 AND EA F-5310-155882 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 550 TO 566, RBL 24 DAMAGED. SEAT TRACK REMOVED AND REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02, REV 105 AND DWG 143N5080 SHT.5 REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 640 RBL 45 CORRODED. R & R WITH SEAT TRACK, FABRICATED IAW DWG 143N5148 SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 143N5085 SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 620 TO 640, RBL 45 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV .105 AND DWG 143N5080 SHT .5 REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 500 TO 520 RBL 24 DAMAGED. SEAT TRACK REMOVED AND REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV.105 AND DWG 143N5080 SHT.5 REV. A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 620 TO 640, RBL 24 DAMAGED. R & R WITH SEAT TRACK FABRICATED IAW DWG 143N5109, SHT.1 REV.A AND INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK BS 440 TO 460, RBL24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK BS 440 TO 460 RBL 24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 143N5080, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1443 TO 1460 TO RBL 45 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02, REV 105 AND DWG 146N5120, SHT 4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1483 TO 1496, RBL 45 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02, REV 105 AND DWG 146N5120 SHT4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (LT WING) · airframe 45,137 hrs · 19,707 cycles
LEFT WING INTERSPAR SKIN L/E UPPER SURFACE, FOUND CORROSION AT WS 688.5 - 691. REPAIRED IAW EA F-5710-155889. REPAIR IS CLASSIFIED AS MINOR.
Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
FWD CARGO LOWER COMPARTMENT BS 740, S25 - 26L, FRAME SPLICE ANGLE CORRODED. FRAME SPLICE ANGLE REMOVED. SPLICE ANGLE FABRICATED IAW DWG 143N1030, SHT 2 REV- AND INSTALLED IAW DWG NR 143N1016, SHT 3, REV D. REPAIR CLASSIFIED AS MAJOR.
Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
FWD CARGO BAY BS 720 S25 - 26L, FRAME SPLICE CORRODED. FRAME SPLICE REMOVED. SPLICE FABRICATED IAW DWG 143N1030, SHT 2, REV- AND INSTALLED IAW DWG 143N1015 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1560 TO 1640, RBL 24 DAMAGED. R & R WITH SEAT TRACK FABRICATED IAW DWG 146N5130, SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 146N5120 SHT4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,137 hrs · 19,707 cycles
FWD CARGO BAY BS 700 S25 - 26L FRAME SPLICE ANGLE CORRODED. FRAME SPLICE ANGLE REMOVED. SPLICE ANGLE FABRICATED IAW DWG 143N1030, SHT 2, REV.- AND INSTALLED IAW DWG 143N1014, SHT 3, REV D. REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1540 TO 1560 RBL 24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 146N5120 SHT 4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 980 TO 1000 RBL 24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK CROWN IAW SRM 51-40-02 REV 105 AND DWG 144N5001, SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 900 TO 960 LBL 45 DAMAGED. R & R WITH SEAT TRACK CROWN FABRICATED IAW DWG 144N5020, SHT 1 REV - AND INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 144N5001 SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 900 TO 960 LBL 24 DAMAGED. R & R WITH SEAT TRACK CROWN FABRICATED IAW DWG 144N5020 SHT 1 REV- AND INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 144N5001 SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1350 TO 1390, RBL 45 DAMAGED. SEAT TRACK F REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02, REV 105 AND DWG 146N5120, SHT 4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — GOUGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
BS 1640 TO 1672, STRINGER 6R, HAS DRILL GOUGES. R & R IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 980 TO 1000 LBL 45 DAMAGED. SEAT TRACK CROWN R & R WITH FABRICATED CROWN IAW SRM 51-40-02, REV 105 AND DWG 144N5001, SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1010 TO 1060, RBL 24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK CROWN IAW SRM 51-40-02 REV 105 AND DWG 144N5001, SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1098 TO 1130, LBL 45 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 144N5001 SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
LEFT CREASE BEAM INNER CHORD APPROX STA 1330 WITH FASTENER HOLE CORRODED AFTER REMOVAL. R & R IAW SRM 51-40-02, REV 105 AND DWG 146N8322, SHT 1, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1400 TO 1430, RBL 45 DAMAGED. SEAT TRACK REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02, REV 105 AND DWG 146N5120, SHT4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1140 TO 1170, LBL 45 DAMAGED. REMOVED AND REPLACED WITH SEAT TRACK FABRICATED IAW DWG 144N5021 SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 144N5001 SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 900 TO 960 RBL 24 DAMAGED. R & R WITH SEAT TRACK FABRICATED IAW DWG 144N5020, SHT 1, REV AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 144N5001 SHT.2 REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1010 TO 1060 LBL 24 DAMAGED. SEAT TRACK R & R WITH FABRICATED SEAT TRACK CROWN IAW SRM 51-40-02, REV 105 AND DWG 144N5001 SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 980 TO 1000, LBL 24 DAMAGED. SEAT TRACK REMOVED AND REPLACED WITH FABRICATED SEAT TRACK CROWN IAW SRM 51-40-02, REV 105 AND DWG 144N5001 SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1010 TO 1060, LBL 45 DAMAGED. SEAT TRACK R & R WITH FABRICATED CROWN IAW SRM 51-40-02 AND DWG 144N5001 SHT 2, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 786 TO 810 RBL 45 HAS DAMAGE. SEAT TRACK R & R WITH FABRICATED SEAT TRACK INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 820 TO 834, LBL 45 HAS SEAT FITTING DAMAGED. R & R WITH SEAT TRACK FABRICATED IAW DWG 143N5106, SHT 1, REV A AND INSTALLED IAW DWG 143N5080 SHT 5, REV A AND SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 1514 TO 1530, RBL 45 DAMAGED. R & R WITH SEAT TRACK FABRICATED IAW DWG 146N5130 SHT 1 REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 146N5120, SHT 4 REV. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 865 TO 870, LBL 45 DAMAGED. SEAT TRACK REMOVED AND REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV.105 AND DWG 143N5080, SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 786 TO 810, LBL 45 HAS DAMAGE. SEAT TRACK REPLACED WITH FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 143N5080, SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 820 TO 834 HAS SEAT FITTING DAMAGED TO CROWN AND CHANNEL. SEAT TRACK REMOVED AND INSTALLED FABRICATED SEAT TRACK IAW SRM 51-40-02 REV 105 AND DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
LEFT CREASE BEAM WEB BETWEEN BS 1300 TO 1320 WITH FASTENER HOLES ELONGATED AT SOME PLACES AFTER REMOVAL. R & R IAW SRM 51-40-02 REV 105 AND DWG 146N8322 SHT 1, REV F. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 500) · airframe 45,137 hrs · 19,707 cycles
LEFT WING UPPER SKIN FOUND CORRODED AT REFUEL FILL PORT AFTER ADAPTOR REMOVAL. REPAIR CARRIED OUT IAW EA F-5730-158161 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 865 TO 870, RBL 45, HAS SEAT FITTING DAMAGED TO CROWN AND CHANNEL. R & R WITH SEAT TRACK FABRICATED IAW DWG 143N5106 SHT1 REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.
Part: SUPPORT — GOUGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK SUPPORT AT STA 365 TO STA 418, RBL 24, STA 407 AND 412 GOUGED. SEAT TRACK SUPPORT R & R IAW DWG 141N5130 SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING ON FRAME AT STA 1280, STR 11R. REPAIRED IAW SRM 53-00-07, REPAIR 3, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING ON FRAME BS 1280, STR 13L. REPAIRED IAW SRM 53-00-07 REPAIR 3 FIG 201 REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFE MARKS ON FRAME FLANGE AT BS 1280 BETWEEN S11-12L. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING MARK ON FRAME AT BS 1280 STR 10L. REPAIR CARRIED OUT IAW SRM 53-00-07 REPAIR 3, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK AT BS 365 TO 418, RBL24 HAS CORROSION ON UPPER CHORD. R & R IAW SRM 51-40-02 REV 105 AND DWG 141N5130, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: SUPPORT — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK SUPPORT AT BS 365 TO 418 HAS ELONGATED HOLE APPROX TO BS 407 POSITION. R & R IAW SRM 51-40-02, REV 105 AND DWG 141N5131, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING ON FRAME AT BS 1280, STR 14L. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: ATTACH FITTING — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
STATION 377.7, LBL 24 SEAT TRACK SUPPORT HAS SHORT EDGE MARGIN ON FLOORBEAM ATTACHING FASTENERS. R & R WITH SEAT TRACK SUPPORT FABRICATED IAW DWG 141N5131, SHT 4 REV D AND INSTALLED IAW DWG 141N5130, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING MARK ON FRAME FLANGE AT BS 1280 AND STR 14R. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG 201 REV.105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FOUND CHAFING ON FRAME AT BS 1280, STR 13R. REPAIRED IAW SRM 53-00-07 REPAIR 3 FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK SUPPORT AT BS 365 TO 418 HAS CORROSION. R & R IAW SRM 51-40-02, REV 105 AND DWG 141N5131, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: SUPPORT — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
SEAT TRACK SUPPORT AT BS 365 TO 418, RBL 24 HAS ELONGATED HOLES IN FLANGE. R & R SEAT TRACK IAW DWG 1415130, SHT 3, REV B. REPAIR IS CLASSIFIED AS MAJOR.
Part: BEAM — CRACKED (CARGO DOOR) · airframe 45,137 hrs · 19,707 cycles
AFT CARGO COMPARTMENT DOOR TOP AFT CORNER EDGE BEAM CRACKED.
Part: BEAM — DENTED (CARGO DOOR) · airframe 45,137 hrs · 19,707 cycles
FWD CARGO DOOR FWD LOWER CORNER BEAM DENTED. REPAIR CARRIED OUT IAW EA F-5230-158198. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FRAME WEB AT BS 418 BETWEEN STR 11R AND STR 12R CHAFED UNDERNEATH STANDOFF AFTER REMOVAL OF STANDOFF. REPAIRED IAW EA F-5310-158163, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — DAMAGED (BS 1640) · airframe 45,137 hrs · 19,707 cycles
CABIN AT BS 1640 STRINGER 4 LEFT HAS A NICK AT FLANGE EDGE. REPAIRED IAW SRM 53-00-03, REPAIR 2, FIG 201, REV.105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
BS 345, LBL 20 TO BL 0 CORROSION ON UNDERSIDE OF FLOORBEAM UPPER TEE AT FASTENER HOLES. R & R WITH FLOORBEAM FABRICATED IAW DWG 141N5121, SHT 4 REV AND INSTALLED IAW SRM 51-40-02 REV 105 AND DWG 141N5111, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHEAR TIE — CHAFED (BS 1440) · airframe 45,137 hrs · 19,707 cycles
AFT CARGO BAY DOOR AT BS 1440, STR 21R INTERNAL FRAME TO EXTERNAL SKIN AFT SURFACE CHAFED. R & R FRAME, FABRICATED IAW DWG 146N6603, SHT 2, REV G AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — NICKED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN AT BS 1320 TO 1340, STR 28 TO 29L HAS NUMEROUS NICKS. REPAIRED IAW EA F-5310-155891, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — NICKED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN AT BS 1360 TO 1380 STR 28R - 29R HAS NUMBEROUS NICKS. REPAIRED IAW EA F-5310-155891, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — NICKED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN AT BS 1340 TO 1360, STR 29R - 30R HAS NUMEROUS NICKS. REPAIRED IAW EA F-5310-155891, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — NICKED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE EXTERIOR SKIN AT BS 1420 TO 1440, STR 26L TO 26R HAS NUMEROUS NICKS. REPAIRED IAW EA F-5310-155891, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — WORN (LT WING) · airframe 45,137 hrs · 19,707 cycles
LEFT WING OTBD L/E NOSE SKIN FOUND WORN JUST OTBD OF NR 1 SLAT, AT OSS 838 TO WBL740. TRIMMED OUT IAW SRM 51- 20-01, REV 105. REPAIR IS CLASSIFIED AS MINOR.
Part: SPLICE — DAMAGED (ZONE 200) · airframe 45,137 hrs · 19,707 cycles
FUSELAGE SKIN BUTT SPLICE AT BS 780 RT BETWEEN STRINGER 4 AND 10 HAS SCRIBE LINE UP TO A DEPTH OF 0.0039". R & R WITH BUTT SPLICE FABRICATED IAW DWG 143N3700 SHT 2, REV A AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
SKIN AT BS 500-520, S27-29R DAMAGED, REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
SKIN AT BS 1470 AT S28L DAMAGED. CARRIED OUT REPAIR IAW EA F-5310-155885, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 45,137 hrs · 19,707 cycles
SKIN AT BS 1520-1540 S27-28L. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 105. REPAIR IS CLASSIFIED AS MAJOR.