N977FD
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORP | Operator | 2023-10-04 – 2023-10-04 | Operator named in NTSB report |
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | 2023-10-04 – 2023-10-04 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFTER INITIAL DEPARTURE RECEIVED MASTER CAUTION TE FLAP DISAGREE. RAN QRH FOR TE FLAP DISAGREE & WERE ABLE TO GET FLAPS TO MATCH HANDLE. RECEIVED MASTER CAUTION L HYD SYS PRESS. RAN QRH FOR LT HYD SYS PRESS, ELECTRICALLY MOVED FLAPS TO 20. ATTEMPTED TO LOWER MLG, NO MOVEMENT OR INDICATIONS OF MOVEMENT. RAN ALTERNATE MLG EXTENSION. EMBEDDED CHKLST IN QRH. ALT GEAR EXTENSION ALSO UNSUCCESSFUL. EMERG DECLARED & AIR RETURN TO CHATTANOOGA, GEAR UP LANDING & ACFT DEPARTING END OF RUNWAY, STRIKING APPROACH LIGHTS & GLIDE SLOPE ANTENNAS. EMERGENCY DECLARED. REMOVED RUPTURED LINE & DELIVERED TO NTSB. INSTALLED TEMP LINE, SERVICED LT HYD SYS. PERFORMED SUCCESSFUL GEAR EXTENSION AS REQUIRED.
L1 DOOR FAILED TO DEPLOY ON EMERGENCY LANDING. A/C HAS BEEN SCRAPPED AND WILL NOT BE REPAIRED CLOSING SDR.
L1 AND R1 DOOR ASSIST BOTTLES BLOWN ON LANDING INTO CHA. A/C HAS BEEN SCRAPPED AND WILL NOT BE REPAIRED. CLOSING SDR
DOT(137-33) MAIN CABIN FLOOR SEAT TRACK FLANGE AT BS 1640 LBL 48 HAS CORROSION. SEAT TRACK ON MAIN CABIN STA 1540 TO 1640 WAS REPAIRED IAW SRM 53-00-52-2R, REPAIR 1, MAJOR REPAIR
TE FLAP ASYM ON CLIMB OUT AFTER SELECTING FLAPS 1. COMPLETED QRH. L AND R FLAP INDICATORS ARE INDICATING BETWEEN 1 AND 5. CONTINUED TO KIND. DECLARED AN EMERGENCY. DID NOT EXCEED MAX FLAP SPEED. ***EMERGENCY DECLARED*** REPLACED RT FLAP POSITION XMITTER PER B757MM 27-58-03-4. PERFORMED ADJUSTMENT TEST OF RT FLAP POSITION XMITTER PER B757MM 27-58-01-5. ALL INICATIONS NORMAL. FLAPS RUN NORMALLY. OK FOR SERVICE.
TE FLAP DISAGREE EICAS MESSAGE ON APPROACH. FLAP HANDLE IN 20 DETENT, FLAP STUCK APPROX 17 DEGREES. NO ABNORMAL ROLL NOTICED. DISCONTINUED APPROACH. RAN QRH AND SELECTED ALTN FLAPS. FLAPS MOVED TO LANDING POSITION. LANDED FLAPS 25. AIRCRAFT ARRIVED EICAS MESSAGE NOT PRESENT, PLACED SYSTEM BACK TO NORMAL CONFIGURATION. CARRIED OUT BITE ON FSEU'S PER FIM 27-51-00 NO CURRENT FAULTS. FOLLOWING FIM 27-51 FT 808 FLAPS DROPPED AND CHECK FLAP TRANSMISSION UNIT OVERLOAD INDICATORS. FOUND #5 TRANSMISSION UNIT INDICATOR TRIPPED. CHECKED FLUID LEVEL ON TRANSMISSION UNIT AND TORQUE LIMITER AS WAS PREVIOUSLY REPLACED. FLUID LEVEL NORMAL. FOUND TRANSMISSION UNITS #2 AND #6 NEEDING FLUID, REQUIRED FLUID NOT AVAILABLE IN JFK. LUBRICATED RIGHT WING TRAILING EDGE FLAP TRACKS AS PER AMM 12-21-09-3 AS SURFACES WHERE DRY. LEFT WING FLAPS STILL REQUIRES LUBRICATIONS. FACT 06APR22 22:55 JFK U SERVICED FLUID LEVEL ON TRANSMISSION #2 AND # 6 PER AMM 12-13-06-3 . LUBRICATED LEFT WING TRAILING EDGE FLAPS PER AMM 21-21-09-3 . NO.5 TRANSMISSION UNIT PLACED ON OIL REF WRI # 27-50/6533 . A/C OK FOR SERVICE
ON APPROACH, LOWERING FLAPS TO 20, WE GOT TE FLAP DISAGREE LIGHT AND EICAS MESSAGE. RAN QRH, USED ALT FLAP SWITCH & LANDED. FLAP LEVER WAS CONFIRMED TO BE IN THE DETENT. INTERROGATED FLAP/SLAT ELEC UNITS #1, #2 & #3 IAW (FIM) 27-51 FAULT TREE 805. INTERROGATED FSEU #1. THERE WERE NO EXISTING FAULTS. FOUND #5 FLAP TANSMMISION TORQUE INDICATOR POPPED. REMOVED AND REPLACE SAME REF B757 MM 27-51-06-4. LEAK AND OPS CHECK GOOD. PERFORMMED EXTEND AND RETACK WITH NO FAULTS AND PERFORMED FLAP TRAMSMITTER CHECK ALL WITH IN LIMITS.
WITH LEFT FMC DEFERRED (REF 34-63/6185) RIGHT AUTOPILOT FAILED IN CRUISE AT FL390 AND WOULD NOT RE- ENGAGE. ALSO VNAV INOP AT THAT POINT. ENROUTE TO MIA CREW ADVISED ALL 3 AUTO PILOTS ARE INOP. DURING LANDING IN MIA CREW EXECUTED A MISSED APPROACH. ON GO AROUND A EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. CRASH, FIRE AND RECUE RESPONDED WITH NO ACTION REQUIRED. REPLACED L FMC AND LOADED SOFTWARE FACTED MEL (REF 34-63/6185) AND PLACED R A/P ON MEL.
ON CLIMB OUT FROM LCK RIGHT MOTOR SHOWED IN THE YELLOW FOR EGT AND ABNORMALLY LOW EPR, ALSO HIGHER THAN NORMAL N1 AND FUEL FLOW; BUT THE THROTTLES WERE STAGGERED WITH THE RIGHT BEING FURTHER AFT. AUTOTHROTTLES KICKED OFF AND WE PULLED THE THROTTLE TO IDLE AND LEFT IT THERE FOR REMAINED OF THE FLIGHT AND IT RAN FINE. DECLARED AN EMERGENCY AND DIVERTED TO KIND. INSPECTED P1 PROBE AND FOUND AN INSECT STUCK INSIDE. DISCONNECTED P1 AIR TUBES AT P1 AIR ACCUMULATOR AND AT FFG AND PURGED SYSTEM WITH DRY NITROGEN. P1 PROBE IS NOW CLEAR AND GOOD AIR FLOW AT ALL POINTS. RECONNECTED AIR TUBES IAW AMM 70-51-00- 2.
MAIN CABIN SEAT TRACK SPLICE AT BL0 IS BOWING UP BETWEEN STA 880 AND 900 ACCOMPLISHED FEDEX EA F-5310-T0360761 TITLE: FUSELAGE - MAIN CABIN FLOOR SEAT TRACK AT BL0 BETWEEN STA 860 AND STA 879 - CORROSION ON FLANGE
L1 DOOR CUTOUT, FWD WEB @ SPRING BALANCER IS GOUGED REMOVED FABRICATED AND INSTALLED WEB IAW BOEING DWG
L/W O/B FLAP O/B TRACK CARRIAGE ASSY 2[EA] INNER PHENOLIC PLATES CRACKED REPAIRED PLATES PER FEDEX EA# F-5750-T0360814-P1
EXTERNAL FUSELAGE UPPER ANTI COLLISION LIGHT ASSY HAS CORROSION REMOVED AND REPLACED UPPER ANTI COLLISION LIGHT IAW AMM 33-44-02-2 OPS CHECK GOOD REF AMM 33-44-02-2
#1 I/B REV INNER AFT PAN CRACKED REPAIRED PER EA #F-7833-T0360755P11RH
#2 ENGINE INBD T/R CASCADE ASSY #16 HAS CORROSION ON MOUNTING FLANGE AT NUTPLATE LOCATIONS REMOVED AND REPLACED #2 ENGINE I/B T/R CASCADE #16 IAW B757 AMM 78-31-05-4.
AFT CARGO COMPARTMENT FLOOR PANEL 161AF HAS MULTIPLE DENTS/GOUGES. MATERIAL FOR NEW AFT CARGO FLOOR PANEL 161AF I.D 2024-T3 .050 CLAD IAW BOEING DRAWING 453N1805 REV W, PO# 991418.1. FABRICATED NEW PANEL IAW BOEING DRAWING 453N1805 REV A. ALODINED AND PRIMED PANEL IAW B757 SRM 51-20-01. PART MARKED PANEL IAW FED EX GMM 07-0-1001 7.B.
#2 ENGINE ,INBOARD THRUST REVERSER, LEADING EDGE, STIFFENER IS CRACKED REMOVED AND REPLACED CRACKED STIFFENER IAW B757 SRM 51-40-02 PAGE 11 AND 12 PARAGRAPH 5 AND ROHR OVERHAUL SHOP DETAIL PARTS REFERENCE 78-31-00
#2 ENGINE INBD TR CASCADE ASSY #9 HAS CORROSION ON MOUNTING FLANGE AT NUTPLATE LOCATIONS. REMOVED AND REPLACED #9 CASCADE ASSY ON #2 ENGINE IB TR IAW B757 AMM 78-31-05-4
LW FIX LE UPPER SURFACE HAS CRACK AT FSS 436- FSS 436 REPAIRED CRACK ON UPPER SURFACE OF L/W FIX L/E PNL WITH 250 DEGREE FIBERGLASS DOUBLER. REPAIR IAW B757 SRM 57- 41-01-2R, 51-70-07-0G 5.A FIG 5 AND B757 AMM 51-21-10-7.
FWD CARGO COMPARTMENT FLOOR PANEL 121BF HAS MULTIPLE GOUGES/DENTS MATERIAL I.D. FOR NEW FLOOR PANEL, FWD CARGO 121BF IS 2024-T3 .050 CLAD P.O. # 994591.1 IAW BOEING DWG 453N1170 REV BN AND B757 SRM 53-30-53 DETAIL VI. FABRICATED PANEL IAW BOEING DWG 453N1170 REV BN, ALODINED AND PRIMED NEW PANEL IAW B757 SRM 51-20-01. PART MARKED PANEL IAW FED EX GMM 07-0-1001 7.B.
AFT CARGO COMPARTMENT FLOOR PANEL 153CF HAS MULTIPLE GOUGES/DENTS FABRICATED NEW 153CF PANEL AFT CARGO USING DWG 453N1805, 2024-T3 .050, P0# 991571.2, LOT # 33780087, PART ID AS -185, ALODINE AND PROTECTIVE COATING IAW B757 SRM 51-20-01 AND DWG 453N1805
(IN COMING WRITE UP) RAMP REPORTED HOLE 1.25 IN FWD CARGO COMPARTMENT FLOOR PANEL 121AF MATERIAL FOR NEW FWD CARGO FLOOR PANEL 121AF I.D. AS 2024-T3 .050 CLAD P.O.# 994591.1 IAW BOEING DWG 453N1170 REV BV. FABRICATED 121AF IAW BOEING DWG 453N1170 REV B. ALODINED AND PRIMED 121AF IAW B757 SRM 51-20-01. PART MARKED 121AF IAW GMM 7-0-1001 7.B.
AFT CARGO FLOOR PANELS HAVE IMPACT DAMAGE BETWEEN BS 1340 - BS 1500 WORK TO BE ACCOMPLISHED ON N//R# 36261/N00261 & N/R# 36262/N00262
WHILE OPENING R1 DOOR , RAFT/ SLIDE COVER CAME OFF AND GOT WEDGED BETWEEN THE AFT DOOR JAMB AND DOOR SLIDE. SLIDE STRAP WAS NOT COMPLETELY TIGHT ALLOWING SLIDE TO SAG. DAMAGED DOOR SLIDE COVER IN PROCESS OF GETTING R1 DOOR OPEN. ACCOMPLISHED REPAIR OF R1 DOOR SLIDE COVER DAMAGE, REF B757 SRM 51-70-20-2R, STEP 5.B. (4)(A) THRU STEP 5.B. (4)(D). REQUIRES SURFACE PREPARATION AND PAINT. SURFACE PREPARED FOR PAINT. APPLIED THE FINISH TO THE REPAIR AREA, PER AMM 25-00-00-7. COVER READY TO PICK UP AT MEM COMP SHOP LEAD BOOTHINSTALLED REPAIRED SLIDE COVER, REF AMM: 25-66-01-4. OK FOR SERVICE.
IN PROCESS OF GETTING R1 DOOR UNSTUCK AND SLIDE IN PROPER POSITION. MANAGED TO BLOW THE R1 DOOR EMERGENCY POWER RESERVOIR. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR BOTTLE, REF AMM: 52-11-30-4. OK FOR SERVICE.
EICAS AND MASTER WARNING EICAS RESOLVED ITSELF BEFORE QRH AND AGENT DISCHARGE COULD BE COMPLETED. UPON ARRIVAL AT SGF, IT WAS NOTED THAT THE FWD AND AFT CARGO COMPARTMENTS WERE LOADED WITH BULK FREIGHT, ALL THE WAY TO THE CEILINGS IN BOTH COMPARTMENTS. THERE WERE NO ALERTS NOR WARNINGS AT BLOCK IN, AND CARGO COMPARTMENT SMOKE DETECTION SYSTEMS TESTED NORMALLY IAW B757 AMM 26-16-00-5-0. FIRE/OVHT LOGIC/TEST PC CARD 6, M10427 IS COMMON TO BOTH THE FWD AND AFT SMOKE DETECTION SYSTEMS. REMOVED AND REPLACED FIRE/OVERHEAT PC CARD ASSY 6, M10427 IAW AMM 26-10-01-4-0. CARGO COMPARTMENT SMOKE DETECTION SYSTEM OPS CKS NORMAL PER AMM 26-16-00-5-0. AC OK FOR SERVICE.
FL360 AFT CARGO FIRE EICAS AND MASTER WARNING EICAS RESOLVED ITSELF BEFORE QRH AND AGENT DISCHARGE COULD BE COMPLETED. REFERENCE WRI 26-12/4866 FOR CORRECTIVE MAINTENANCE ACTION AND REMOVE/INSTALL PARTS INFO FOR THIS WRI, ALSO. ALL INFO APPLIES TO BOTH ITEMS. AC OK FOR SERVICE.
REPEAT WRITE UP. REJECTED TO AT 60KTS FMC MESSAGE "TAKEOFF SPEEDS DELETED" TAKEOFF SPEEDS DISAPPEARED. MULTIPLE EICAS CAUTIONS INCLUDING AUTOTHROTTLE, FUEL CONFIG, TAT PROBE AND PROBE HEAT. REMOVED AND REPLACED NR 1 TRU.
REJECTED TAKEOFF INITIATED AT 40 KTS. MUTIPLE CAUTION EICAS ALERTS INCLUDING PROBE HEAT, R FWD FUEL PUMP, AUTOTHROT DISC AND L YAW DAMP. TAKEOFF SPEEDS ALSO DELETED. REMOVED AND REPLACED NR 1 TRU.
ON CLIMB OUT CABIN AUTO MESSAGE APPEARED. TRIED TO FOLLOW QRH AND MANUALLY SET PRESSURE BUT THAT DID NOT WORK. FOUND AND REPAIRED DAMAGED WIRING NEAR OUTFLOW VALVE. SPLICED IN NEW SHIELDED WIRE PAIR W2632-2501R/B-24 AND NEW TWISTED PAIR W2632-2008B/R-20 APPROX 5 FEET AWAY FROM CONNECTOR AND ROUTED AND TERMINATED AT CONNECTOR D2336 REF SWPM 20-10-13, SWPM 20-10-11 AND WDM 21-31-21 SHEET 2. RESECURED ALL WIRING. UPON POWERING UP AIRCRAFT- NO STATUS MESSAGES PRESENT. BITE CHECKED BOTH CPC CONTROLLERS REF AMM 21-31-02-4 AND PERFORMED OUTFLOW VALVE ACTUATOR TEST REF AMM 21-31-04-4. NO FAILURES. MANUAL FUNCTION OPERATES NORMAL. "AUTO INOP" LIGHT ON OVERHEAD IS NOT ILLUMINATED. ISFD INDICATOR. PERFORMED ADJ/TEST ON THE ELECTRONIC STANDBY INSTRUMENT SYSTEM (ESIS) PER MM 34-24-00-5-99, NO FAULTS NOTED. ALSO, PERFORMED PRESSURIZATION CONTROL SYS ADJ/TEST ON BOTH SYSTEMS PER MM 21-31-00-5. OPS CHECK NORMAL A/C OK FOR SERVICE.
ON DESCENT THROUGH FL210 AIRCRAFT BELOW VNAV PATH A/C AGGRESIVELY PITCHED OVER. CREW WENT TO V/S 1100 FPM AND A/C PITCHED OVER TO ROUGHLY 5900 FPM. CREW DISCONNECTED A/P (RIGHT A/P WAS ENGAGED) CREW TRIED CENTER A/P SELECTED V/S 600 FPM A/C PITCHED OVER AGAIN TO 5000 FPM. TRIED LEFT A/P V/S AND A/C PITCHED OVER AGAIN -DISCONNECTED A/P AGAIN. T/S PER FIM 34-61-00-815-823-0, WITH NO DEFECTS FOUND. PERFORMED MCDP FAULT REVIEW PER MM 22-00-02-2, NO DEFECTS RELATED TO CURRENT WRI SINCE FLIGHT LEG 56 & HIGHER. REMOVED AND REPLACED MCP PRECAUTIONARY PER MM 22-11-02-2, OPS CHECKS GOOD. PERFORMED MCDP TESTS: 04, 30, & 40 WITH NO DEFECTS NOTED PER MM 22-00-02-2. A/C OK FOR SERVICE.
IN DECENT FROM FL340 TO 14000, CLEAN CONFIG, PASSING APPROX FL 190 A/C PITCHED NOSE DOWN TO APPROX 9, AIRSPEED STARTED TO INCREASE INTO ZIPPER APPROX 5 KTS FOR 5 SEC UNTIL AP WAS DISCONNECTED AND SPEEDBRAKES DEPLOYED. INSPECTED AIRCRAFT NO ABNORMALITIES NOTED PER AMM 05-51-04-2-0, A.C OK FOR SERVICE
RT FUSELAGE HAS GOUGE AT STA. 218, JUST BELOW STR. 23R EVALUATED DAMAGE AT STA 218 JUST BELOW STR 23R FOUND TO BE DENT WITH GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET III. CUTOUT DAMAGE DIM 1.6" X 1.4" AND REPAIRED IAW SRM 53-00-01-2R REPAIR 16 REWORK REQUIRED REF: REWORK SNRM N00523.
EXTERIOR BATTERY POWERED EMERGENCY LIGHT LOCATED AFT OF R-1 MAIN ENTRY DOOR INOP. REMOVED AND REPLACED LAMP ON R1 DOOR EXTERNAL SLIDE LAMP IAW B757 AMM 33-51-06-2-1OPS CK SATIFACTORY R1 DOOR EXTERNAL SLIDE LAMP IAW B757 AMM 33-51-06-2-1
PDIS 977 25-60 3952 16JAN19 GSO OPEN U LOGPAGES:2922410 RED SLIDE ARMED INDICATOR DOES NOT EXTEND FULLY WHEN THE DOOR IS ARMED (L1 DOOR) FACT 16JAN19 14:48 ORD APPLIED DC-33 TO GIRT BAR FLOOR FITTINGS AND REPOSITIONED UPPER DOOR LINER. PERFORMED OPS. CHECK OF GIRT BAR AND DOOR SLIDE ARMING PER MM 52-11-25 .OPS. CHECKED NORMAL.
AT LEVEL OFF CTR L FUEL PUMP PRESS LIGHT ILLUMINATED. RAN QRH NO HELP DUE TO R CTR FUEL PUMP MEL'D. FUEL TRAPPED WAS 6500LBS UNABLE TO BALANCE FUEL0 RTB TO KMEM. EMERGENCY DECLARED. TRANSFERRED FUEL INTO CENTER TANK FROM LEFT AND RIGHT, TOTAL FUEL IN CENTER TANK WAS 20,200 TO PROPERLY PRIME THE PUMP. RAN ENGINES JUST USING CENTER LEFT FUEL PUMP AND PUMP OPS CHECKED GOOD. DUE TO HISTORY FOR LEFT CENTER PUMP PRESSURE LIGHT NOT GOING OUT WHEN ON. REMOVED AND REPLACED CENTER. LEAK AND OP CHECKED CENTER LT BOOST PUMP PRESSURE SWITCH REF AMM 28-42-01-4-1. LEAK AND OP CHECK GOOD. LEFT FUEL PRESSURE SWITCH REF AMM 28-42-01-4-1.
AFTER DEPARTING, WHEN MOVING FLAPS FROM FLAPS 1 TO FLAPS UP, RECEIVED AN LE SLAT ASSYMETERY. EMERGENCY DECLAIRED, RAN QRH, RETURNED TO DEPARTURE. REMOVED AND REPLACED THE LT OTBD SLAT LOSS SENSING SWITCH IAW MM 27-81-42-4. ADJUSTED SWITCH IAW MM 27-81-42-5. ISOLATED THE INBD AND OTBD SLAT LOSS SWITCHES. MEGGED ALL WIRES IN WINGS AND FUSELAGE. NO SHORTS TO GROUND NOTED. ACCOMPLISHED AN ADJUSTMENT TEST OF THE OTBD SLAT LOSS SWITCHES IAW 27-81-42-5. OPS CHECKED GOOD.
LE FLAP ASYMMETRY ON APPROCH. COMPLIED WIHT QRH. CONTINUED TO UNEVENTFUL LANDING. PERFORMED BITE CHECK OF FSEU NR 1, 2, & 3. FOUND SLAT LOSS ON LEG 0 AND SLAT DISAGREE ON LEG 1 OF FSEU NR 1. FOUND SLAT LOSS/SLAT SYSTEM ON FSEU NR 2. NO FAULTS ON FSEU NR 3. TROUBLESHOT IAW FIM 27-81/ FT 804. CHECKED D41828P PIN 7 FOR GROUND, FOUND OPEN. CHECKED D41630P PIN 7 FOR GROUND, ALSO FOUND OPEN. CHECKED PIN G9 OF CONNECTOR D3312A FOR GROUND, FOUND OPEN. R & R THE LEFT AND RIGHT SLAT POSITION TRANSMITTERS IAW AMM 27-88-01-4. OPS CHECKED GOOD.
ON FINAL APPROACH, LE FLAP ASYMETRY EICAS MESSAGE WITH LEADING EDGE LIGHT. ACCOMPLISHED LE FLAP ASYMETRY CHECKLIST AND LANDED UNEVENTFULLY. INSTALLED A LT INBD SLAT LOSS SWITCH NON ADJUSTABLE TRACK IAW AMM 757-27-81-41-5. CYCLED SLATS THROUGH SEVERAL CYCLES WITH NO FAULTS.
TRAILING EDGE FLAP DISAGREE MASTER CAUTION ON SHORT FINAL. EXECUTED A GO AROUND. COMPLIED WITH QRH LANDED FLAPS 20 KPWM. ONCE DOWN POWERED RETRACTED FLAPS, PER FIM 27-51-00 FT 808. CHECKED FSEU NO "LRU" FAULTS. RETURN A/C TO NORMAL CONFIGURATION.
EICAS FOR ANTI SKID, NUMEROUS TIMES DURING FLIGHT REMOVED & REPLACED THE ANTI-SKID, AUTOBRAKE CONTROL UNIT ASSY, OPS CHECKED NORMAL IAWAMM 32-42-01-4.
LEFT ENTRY DOOR SLIDE LIGHT INOPERATIVE. TROUBLESHOT TO STATIC LINE CAUGHT IN GIRT BAR. UNTANGLED THE STATIC LINE & TUCKED INTO FOLDED GIRT BAR SLIDE POUCH IAW AMM 25-66-01-4.
LEFT ENTRY DOOR WILL NOT CLOSE PROPERLY. FOUND LOOSE LANYARD INTERFERRING WITH GIRT BAR. RESTOWED LANYARD IAW AMM 25-66-01-4. OPS CHECK SATISFACTORY.
GROUND POWER RECEPTACLE PAN, HAS ONE GOUGE ON STIFFENER. REMOVED, FABRICATED, AND INSTALLED THE NEW STIFFENER IAW SRM 51-40-02-0G, DWG 141N8271 REV. R AND REV. E. MAJOR REPAIR.
E & E BAY. EXTERNAL GROUND POWER RECEPTACLE PAN HAD TWO UPPER RECEPTACLE FITTING MOUNT HOLES CRACKED. REMOVED AND REPLACED THE EXTERNAL GROUND POWER RECEPTACLE PAN, COMPLIED WITH EA F-5240-T0331639 P1. THIS IS A MAJOR REPAIR.
COULD NOT GET SLIDE TO ARM AFTER CLOSING L1 DOOR. PERFORMED AN OPS CHECK OF DOOR AND SLIDE ARMING. OPS CHECKED GOOD IAW AMM 52-11-00-5.
L1 DOOR WILL NOT ARM PROPERLY.
L1 DOOR EMERGENCY POWER RESERVOIR GAUGE IS SHOWING EMPTY. R & R L1 DOOR OPEN RESERVOIR; NO LEAKS NOTED, RII PROCEDURES C/W REF AMM.
L1 SLIDE FELL OUT OF DOOR. DOOR WAS NOT ARMED. SLIDE DID NOT DEPLOY. R & R L1 DOOR ESCAPE SLIDE AND GIRT BAR IAW AMM 25-66-01-4. OK FOR SERVICE, GIRT BAR REMOVED, PN 140N2762-17, SN LTD5482, SLIDE, RAFT REMOVED PN D30654-122, SN 1253RP.
UPON ARRIVAL, L1 DOOR EMER SLIDE FELL OF THE DOOR & UPON FURTHER INSPECTION FOUND LT NR 1 DOOR ASSIST DISCHARGED. REINSTALLED NR 1 LT PAX DOOR SLIDE IAW MM CHAPTER 52-11-04-4, ALSO INSTALLED DOOR GUIDE IAW MM CHAPTER 52-11-04-2. OPERATIONS CHECKED NORMAL. ACFT SILL REQUIRES DOOR OPEN ASSIST INSTALLATION. R & R L1 LT DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-4. PERFORMED INSPECTION & CHECK IAW AMM 52-11-30-6.
AT FL 380, FLAP GAUGE INDICATED 1/2 & RECEIVED, FLAP LIM, FMA ON PFD. FLAP HANDLE WAS NOT MOVED, ALSO RECEIVED, FLAP & SLAT ELEC STATUS. WHEN WE SLOWED & THE ATTEMPTED TO CONFIGURE FOR LANDING, RECEIVED TE FLAPS ASYMMETRY, EICAS & TE, DISCRETE LIGHT. CONDUCTED QRH & RESULT WAS SLATS OUT FLAPS UP LANDING. REPLACED L/H FLAP POSITION TRANSMITTER IAW MM 27-58-03 AND PERFORMED ADJUSTMENT TEST IAW MM 27-58-01 NO FAULTS, SYSTEM CHECKED NORMAL. ALSO PERFORMED FSEU OPS CHECK IAW MM 27-51-01 NO FAULTS ON FSEU'S. ALL PANELS REINSTALLED.
DURING DESCENT, RECEIVED EICAS TE ASYM, TE DISCRETE LIGHT & FLAP GAUGE BOTH NEEDLES INDICATED 1/2 WAY BETWEEN UP & 1. SPEED WAS 320 KNOTS & ALTITUDE WAS 21,500. WE SLOWED BELOW 240 KNOTS & READ QRH PROCEDURE. LANDED WITH SLATS EXTENDED & FLAPS UP. ONCE ACFT SLOWED, FLAP GAUGE INDICATED NORMALLY, BUT EICAS MSG & DISCRETE LIGHT REMAINED. TROUBLE SHOT IAW FIM 27-51 FIG 809. FOUND NUMEROUS FAULTS ON NR 1 FSEU. R & R NR 1 FSEU IAW AMM 27-51-01. OPERATIONS CHECKED NORMAL, NO FURTHER FAULTS.
TEST FLIGHT, R1 DOOR SLIDE, ARMED SEGMENT LIGHT INOPERATIVE. RE LAMPED BULBS IN R1 SLIDE LIGHT ASSEMBLY IAW AMM 33-16-02-2. TESTED GOOD IAW AMM 33-22-00-5.
TEST FLIGHT, RT EMER DOOR EICAS MSG POSTED THROUGHOUT THE ENTIRE FLIGHT. ADJUSTED RT EMER DOOR SWITCH IAW AMM 52-71-00-5. CHECKED GOOD.
FORWARD CARGO COMPARTMENT BS 740, STRINGER 26 - 27R FRAME UPPER FLANGE HAS CORROSION. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. MAJOR REPAIR.
LEFT PYLON, NACELLE STATION 201.02, BULKHEAD AFT LT EDGE FOUND GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 54-51-02, FIG. 101, DETAIL V. REPAIRED IAW EA F-5450-T0314207, PT 1. MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 19R FROM BS 660 - BS 680 & FROM BS 740 - 780 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM, REQUIRING ADDITIONAL STRIPPING FROM BS 660 - 780. COMPLIED WITH EA F-5330-T0310055. TITLE FUSELAGE, PLATES & SKINS SECTION 43, SCRIBE LINE & CORROSION REPAIR STATION 661 - 781 STRINGER 19R, DATED SEP 25 2014. MAJOR REPAIR.
REWORK OF NON-ROUTINE N02513 FUSELAGE CORROSION FOUND ON SKIN RUNNING UNDER LAP SEAM STRINGER 26R STATION 660 - 900 DUE TO DOUBLER REPAIR HAVING MULTIPLE DENTS. REMOVED DAMAGED DOUBLER REPAIR IAW SRM 51-40-02. FABRICATED & INSTALLED A NEW DOUBLER REPAIR IAW EA F-5330-T0310316 P1 STEPS 16 TO 26, INSTRUCTIONS WITH REFERENCE TO NR N02513. FIRST STAGE APPROVAL ONLY. MAJOR REPAIR CAT B.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 26L FROM BS 661 TO 720 WITH CORROSION ON TOP OF SCRIBE LINE. REPAIRED IAW EA F-5330-T0313764. MAJOR REPAIR.
LAP JOINT 26R INCLUDING TRANSITION UNDER AFT CARGO HAS BUBBLED PAINT & SIGNS OF CORROSION BS 1400 - 1460. REPAIRED IAW EA F-5330-T0313396. MAJOR REPAIR.
LAP JOINT STRINGER 20R BS 199 - 440 HAS NUMEROUS AREAS OF BUBBLED PAINT & EVIDENCE OF CORROSION. REPAIRED IAW EA F-5310-T0311288.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 14L FROM BS 760 - 780 & UP TO THE AFT EDGE OF HALO SHORING. REPAIRED IAW EA F-5330-T0312066.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 26R FROM BS 1520 TO 1610 REQUIRING ADDITIONAL STRIPPING FROM BS 1460 TO 1620. REPAIRED IAW EA F-5330-T0313107. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 26L FROM BS 1480 TO 1620 WITH CORROSION ON UPPER SKIN SURFACE. REPAIRED IAW EA F-5330-T0312987. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 20R FROM BS 1470 TO 1500 REQUIRING ADDITIONAL STRIPPING FROM BS 1460 TO 1620. COMPLIED WITH EA F-5330-T0312993. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 14R FROM BS 440 - 540 WITH CORROSION ON UPPER SKIN SURFACE. REPAIRED IAW EA F-5330-T0312933.
FOUND SCRIBE LINE IN UPPER FWD CROWN DECAL AREA FROM BS 816.125 TO 817.375 1 INCH BELOW STRINGER 3L. COMPLIED WITH EA F-5330-T0308151 PT 1 FUSELAGE PLATES & SKINS EO F-5330-7-5000 PT 5 DECAL ZONE 4 SCRIBE LINE INSPECTIONS. MAJOR REPAIR.
FOUND SCRIBE LINE IN UPPER FWD CROWN DECAL AREA FROM BS 842.250 TO 844.375 10 INCHES BELOW STRINGER 3R. COMPLIED WITH EA F-5330-T0308151 PT 1 FUSELAGE PLATES & SKINS EO F-5330-7-5000 PT 5 DECAL ZONE 4 SCRIBE LINE INSPECTIONS. MAJOR REPAIR.
FOUND SCRIBE LINE IN UPPER FWD CROWN DECAL AREA FROM BS 886.063 TO 889.750 10 INCHES BELOW STRINGER 3R. COMPLIED WITH EA F-5330-T0308151 PT 1 FUSELAGE PLATES & SKINS EO F-5330-7-5000 PT 5 DECAL ZONE 4 SCRIBE LINE INSPECTIONS. MAJOR REPAIR.
FOUND SCRIBE LINE IN UPPER FWD CROWN DECAL AREA RUNNING VERTICAL AT BS 712.875 10.5 INCHES BELOW STRINGER 3L. COMPLIED WITH EA F-5330-T0308151 PT 1 FUSELAGE PLATES & SKINS EO F-5330-7-5000 PT 5 DECAL ZONE 4 SCRIBE LINE INSPECTIONS. MAJOR REPAIR.
EXTERNAL FUSELAGE SKIN BS 199 - 297 STRINGER 20L LAP SEAM HAS EVIDENCE OF CORROSION. REPAIRED IAW EA F-5330-T0311102.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 20L FROM BS 1186 TO 1460 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM FROM BS 1280 TO 1460 REQUIRING ADDITIONAL STRIPPING FROM BS 1180 TO BS1460. SDR 14-3481 WAS GEN IN ERROR. DUPLICATE WRITE UP. PLS SEE SDR 14-2671. COMPLIED WITH EA F-5330-T0309329 DATED 10/08/2014. TITLE FUSELAGE PLATES & SKIN CORROSION REPAIR & SCRIBE LINE LRTS AT LAP JOINT STATION 1180 TO 1460 STRINGER 20L.
EXTERNAL FUSELAGE SKIN BS 900 - 1180 STRINGER 4R LAP SEAM HAS PAINT PEELING WITH CORROSION. REPAIRED IAW EA F-5330-T0312281.
CORROSION BLEND AT STRINGER 20L LAP JOINT BETWEEN STATION 297 & 439. COMPLIED WITH EA F-5330-T0312078 PT 1. TITLE FUSELAGE, PLATES & SKINS REPAIR TRACKING STRINGER 20L LAP JOINT, STATION 297 & 439 DATED OCT 02 2014. MAJOR REPAIR CAT B.
MAIN & CTR TANK FUEL PUMP BONDING JUMPER RT FRONT SPAR WEB CORRODED. WORK ACCOMPLISHED ON EA F-5710-T0311760. WINGS BASIC WING STRUCTURE RT WING FRONT SPAR CORROSION, FSS 172.92 RT SIDE, FWD BOOST PUMP SB757-28-0110, MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 4L FROM BS 1460 - 1620. ACCOMPLISHED EA F-5330-T0312060 PT 1. MAJOR REPAIR.
FOUND CORROSION ON SKIN RUNNING UNDER LAP SEAM AT STRINGER 26L FROM BS 1636 - 1662. REPAIRED IAW EA F-5330-T0309699 PT 1. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 4R FROM BS 1460 TO 1620. ACCOMPLISHED EA F-5330-T0311902 FUSELAGE PLATES & SKINS CORROSION REPAIR TRACKING LAP SEAM STRINGER 4R STATION 1459 - 1620. MAJOR REPAIR.
WHILE PERFORMING VISUAL INSPECTION LAP SEAM FOUND STRINGER 27R BETWEEN BS 660 - 668 DAMAGED. NO ALLOWABLE DAMAGES ARE ESTABLISHED ON SRM FOR ACFT STRINGERS. REPLACED DAMAGED STRINGER SECTION IAW SRM 53-00-03 FIG 201 REPAIR 2.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 4L FROM BS 1320 TO 1360 & FROM BS 1400 TO 1460 REQUIRING ADDITIONAL STRIPPING FROM BS 1180 TO 1460. ACCOMPLISHED EA F-5330-T0312157 FUSELAGE PLATES & SKINS CORROSION REPAIR TRACKING STRINGER 4L LAP JOINT STATION 1180 - 1459. MAJOR REPAIR.
AFT PIT STATION 1480 STRINGER 26R FRAME IS CORRODED ON FWD SIDE. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA ORIG MATERIAL .063 MATERIAL REMAINING .055 D=.008 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. R & R FRAME STATION 1480 STRINGER 23L TO 23R BATCH 0002690754 PN 146N1030-76 IAW SRM 51-40-02 & DWG 146N1015. MAJOR REPAIR.
FUSELAGE EXTERNAL SKIN LAP JOINT AT STRINGER 10R FROM BS 1460 TO 1620 HAS AREAS WITH BULGING PAINT & SIGNS OF CORROSION. ACCOMPLISHED EA F-5330-T0312009 FUSELAGE PLATES & SKINS CORROSION REPAIR TRACKING STRINGER 10R LAP JOINT STATION 1460 - 1620. MAJOR REPAIR.
RIGHT ELEVATOR FRONT SPAR MIDDLE PCA ROD END HINGE FITTING LUG GOUGED BETWEEN RIB 7 & 8. STABILIZER ELEVATORS RT ELEV ACTUATOR FITTING LUG EDGE DAMAGE ELEV STATION 136.532 & 160.525 WORK ACCOMPLISHED IAW EA F-5520-T0311146. MAJOR REPAIR.
RIGHT ELEV OTBD PCA ROD END ATTACHMENT FITTING HAS NICKS & GOUGES. STABILIZERS ELEVATORS RT ELEV ACTUATION FITTINGS LUG EDGE DAMAGE ELEV STATION 136.532 & 160.525. WORK ACCOMPLISHED IAW EA F-5520-T0311146. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 4R FROM BS 1340 TO 1360 & BS 1400 TO 1460 REQUIRING ADDITIONAL STRIPPING FROM BS 1180 TO 1460. ACCOMPLISHED EA F-5330-T0311973 FUSELAGE PLATES & SKINS CORROSION REPAIR TRACKING LAP JOINT AT STRINGER 4R BETWEEN STATION 1180 - 1460 MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 14R FROM BS 661 TO 781. ACCOMPLISHED EA F-5330-T0311700 FUSELAGE PLATES & SKIN CORROSION REPAIR. MAJOR REPAIR.
AFT CARGO BAY STRINGER 28R HAS CORROSION ON INBD SIDE AT BS 1340. CLEANED AREA, AND FOUND OUT OF LIMITS IAW SRM 53-00-03. INSTALLED REPAIR IAW SRM 53-00-03 FIG 201 DET 3 REPAIR 2. MAJOR REPAIR..
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 4R FROM BS 700 TO 781 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM & WITH CORROSION ON UPPER SKIN SURFACE AT MARKED LOCATIONS REQUIRING ADDITIONAL STRIPPING FROM BS 661 - 700. COMPLIED WITH EA F-5330-T0310097 PT1 TITLE PLATES & SKINS FUSELAGE SEC 43 SCRIBE LINE & CORROSION REPAIR STATION 661 TO 781 STRINGER 4R. MAJOR REPAIR.
RIGHT TUNNEL AREA AT BS 365 NLG WW WALL STIFFENER HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. CHECK LIMIT ORIGINAL MATERIAL .120 MATERIAL LOSS .039. FOUND OUT OF LIMITS IAW SRM 53-10-14 FIG 101 DETAIL II. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02 AND DWG 141N9951. MAJOR REPAIR.
LAP JOINT 14R BS 1620 - 1650 HAS AREAS OF BUBBLED PAINT & EVIDENCE OF CORROSION. COMPLIED WITH EA 757-5361-16-F4736 FOR CORROSION AT LAP JOINT 14R BS 1620 - 1650, NO DEVIATIONS NOTED. IAW EA F-5330-T0311765 FUSELAGE PLATES & SKINS CORROSION REPAIR TRACKING LAP SEAM STRINGER 14R STATION 1620 - 1640. MAJOR REPAIR.
FUSELAGE EXTERNAL SKIN LAP JOINT AT STRINGER 10L FROM BS 1180 - 1460 FOUND WITH BULGING PAINT & SIGNS OF CORROSION. REPAIRED IAW EA F-5330-T0311206. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 14R FROM BS 1240 TO 1300. REPAIRED IAW EA F-5330-T0310537 PT 1.
FUSELAGE EXTERNAL SKIN LAP JOINT AT STRINGER 10R FROM BS 1180 TO 1460 HAS AREAS WITH BULGING PAINT & SIGNS OF CORROSION. REMOVED CORROSION & ACCOMPLISHED EA F-5330-T0311056. FUSELAGE PLATES & SKIN AT LAP JOINT STATION 1180 TO 1460, STRINGER 10R. MAJOR REPAIR.
NR 2 PYLON FWD RT LOWER MID BULKHEAD FLANGE HOLE CAME IN WITH A 1ST OVERSIZE BOLT. ACCOMPLISHED EA F-5450-T0311100 NACELLES & PYLON, PYLONS STRUCTURES, NR 2 PYLON FWD RT MID BULKHEAD, OVERSIZE FASTENER REWORK. MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 4L FROM BS 700 TO 781 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM REQUIRING ADDITIONAL STRIPPING FROM BS 661 TO 700. ACCOMPLISHED EA F-5330-T0310069 FUSELAGE PLATES & SKINS SECTION 43 SCRIBE LINE & CORROSION REPAIR STATION 661 - 781 STRINGER 4L. MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT 20L FROM BS 1186 TO 1460 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM FROM BS 1280 TO 1460 REQUIRING ADDITIONAL STRIPPING. REPAIRED IAW EA F-5330-T0309329.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 19L FROM BS 660 TO 680 & BS 740 TO 770 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM REQUIRING ADDITIONAL STRIPPING. ACCOMPLISHED EA F-5330-T0310315 FUSELAGE PLATES & SKINS, SECTION 43 SCRIBE LINE & CORROSION REPAIR STATION 661 TO 780 STRINGER 19L. MAJOR REPAIR.
INCOMING CONDITION SCRIBE LINE AT STRINGER 26L FROM STATION 440 - 661. A SCRIBE LINE REPAIR WAS ACCOMPLISHED ON NR 6000236731001 & EA 757-5331-16-F4576. IAW EA F-5330-T0310041 TITLE FUSELAGE PLATES & SKINS SECTION 43 SCRIBE LINE CORROSION REPAIR STATION 440 - 661 STRINGER 26L DATED SEPT 12, 2014 & FAA FORM 8110-3 DATED MAY 12, 2014. NON-ROUTINE IS FOR TRACKING PURPOSES ONLY CAT A MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 10R FROM AFT EDGE OF R4 DOOR TO BS 1720 REQUIRING ADDITIONAL STRIPPING FROM BS 1620 TO FWD EDGE OF R4 DOOR. ACCOMPLISHED EA F-5330-T0309233 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION REPAIR AT LAP JOINT STATION 1621 TO 1720 STRINGER 10R & 10L. THIS IS A CAT B REPAIR.
RIGHT WING TO STRUT ATTACHMENT OTBD SIDE LOAD FITTING HAS A MIGRATED BUSHING. ACCOMPLISHED EA F-5740-TO310226 WINGS ATTACH FITTINGS RT WING TO STRUT ATTACHMENT MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 10L FROM AFT EDGE OF L4 DOOR CUT OUT TO BS 1720. ACCOMPLISHED EA F-5330-T0309233. THIS IS A CAT B REPAIR.
FORWARD CARGO BY BILGE AREA LOWER STRINGER 28L ANGLE BETWEEN BS 760 - 800 HAS CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-12 PG 102 FIG 101 DETAIL IV. INSTALLED REPAIR IAW SRM 51-70-12.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 26R FROM BS 500 TO 520 & FROM BS 540 TO 560 REQUIRING ADDITIONAL STRIPPING FROM BS 440 TO 660. ACCOMPLISHED EA F-5330-T0309678. FUSELAGE PLATES & SKINS CORROSION LAP SEAM STRINGER 26R STATION 439 - 661. THIS IS A CAT A REPAIR.
AFT CARGO COMPARTMENT BETWEEN BS 1580 - 1600 AT STRINGER 29R, STRINGER CORRODED AS MARKED. REMOVED CORROSION IAW SRM 51-10-02. NO ALLOWABLE DAMAGE FOR AIRPLANE. REPAIRED STRINGER STATION 1530 RT TO 1620 RT IAW SRM 53-00-03 REPAIR 2. CAT A MAJOR REPAIR.
BS 781 STRINGER 14R SPLICE STRAP HAS CORROSION. REMOVED CORROSION FROM SPLICE STRAP AT BS 781 STRINGER 14R IAW SRM 51-10-02. NO ALLOWABLE DAMAGE ON SPLICE STRAP IAW SRM 53-00-11 FIG 101 DETAIL V. R & R SPLICE STRAP FROM BS 781 STRINGER 10R TO STRINGER 14R IAW SRM 51-40-02. CATEGORY A MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDERLAP SEAM AT STRINGER 20L FROM BS 1620 TO STRINGER 1720. ACCOMPLISHED EA F-5330-T0309060 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION REPAIR AT LAP JOINT STATION 1620 TO 1720 STRINGER 20L. CATEGORY B MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDERLAP SEAM AT STRINGER 20R FROM BS 1620 TO 1720. ACCOMPLISHED EA F-5330-T0309169 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION AT LAP JOINT STATION 1621 TO 1720 STRINGER 20R. CATEGORY A MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 26R FROM BS 660 - 710. REPAIRED IAW EA F-5330-T0310316.
NUMBER 2 PYLON INTERNAL LT SIDE, PP STATION 174 SKIN CORRODED. ACCOMPLISHED EA F-5450-T0308182 NACELLES / PYLON - PYLONS STRUCTURES - NR 2 STRUT LT AFT SKIN PANEL CORRSION. CATEGORY "A" MAJOR REPAIR
FUSELAGE EXTERNAL SKIN LAP JOINT AT STRINGER 10R FROM BS 375 TO 440 FOUND WITH CORROSION AS MARKED. A REPAIR WAS ACCOMPLISHED ON VT MAE WC 6000236749 & EA 757-5311-16-F4670 REV DATED JULY 23, 2014 & FORM 8110-3 DATED JULY 24, 2014 ATTACHED IAW EA F-5330- T0310105. FUSELAGE PLATES & SKINS, CORROSION REPAIR STATION 365 TO 439 STRINGER 10R LAP JOINT STC HOLDER EA 757-5311-16-F4670. THIS NON-ROUTINE FOR TRACKING PURPOSES. MAJOR REPAIR.
FUSELAGE EXTERNAL SKIN LAP JOINT AT STRINGER 10L FROM BS 375 TO 440 FOUND WITH CORROSION AS MARKED. A REPAIR WAS ACCOMPLISHED ON VT MAE WC 6000236750 & EA 757-5311-16-F4669 REV DATED JULY 23, 2014 FORM 8110-3 DATED JULY 24, 2014 IAW EA F-5330-T0310166. FUSELAGE PLATES & SKIN, CORROSION REPAIR STATION 375 TO 440, STRINGER 10L LAP JOINT. STC HOLDER EA 757-5311-16-F4669. THE NON-ROUTINE FOR TRACKING PURPOSES. MAJOR REPAIR.
INCOMING, NR 3 CARGO DOOR SKIN DENT TWO EA APPROX AFT AREA OF DOOR. AFTER FURHER DENT EVALUATION DENT NR 1 WAS FOUND WITHIN LIMITS IAW SRM 52-30-01 FIG 101 DETAIL VI. DENT NR 2 WAS FOUND OUT OF LIMITS IAW SRM 52-30-01 FIG 101. DETAIL VI DENT NR 2 WAS REPAIRED IAW SRM 52-30-01 REPAIR NR 4 ACCOMPLISHED ON EA F-5230-T0311449 DOORS - NR 3 CARGO DOOR. MAJOR REPAIR
UPPER FUSELAGE SKIN BS 297.0 - 333.45 CORRODED ON LAP SEAM. REPAIRED IAW EA F-5330-T0310009. CATEGORY "A" MAJOR REPAIR.
FUSELAGE EXTERIOR SKIN STATION 900 - 1180 STRINGER 10L LAP SEAM CORRODED. REPAIRED IAW EA F-5340-T0310072A. MAJOR REPAIR.
UPPER FUSELAGE SKIN BS 900 - 1180 STRINGER 10R LAP SEAM HAS CORROSION. REPAIRED IAW EA F-5340-T0310075A. MAJOR REPAIR.
AFT CARGO STRINGER 28RT HAS EXFOLIATED CORROSION ON OTBD SIDE STATION 1600, NOTED WHEN SKIN REMOVAL. R & R AFT CARGO STRINGER 28RT ON OTBD SIDE IAW SRM 51-40-02, STATION 1580 - 1600. CATEGORY A MAJOR REPAIR.
LEFT FUSELAGE SKIN BETWEEN BS 940 - 960 STRINGER 4L CORRODED. REPAIRED IAW EA F-5330-T0310003. CATEGORY B MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 14L FROM BS 780 TO 800 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM WITH CORROSION ON UPPER SKIN SURFACE AT MARKED LOCATIONS REQUIRING ADDITIONAL STRIPPING FROM BS 780 TO 900. REMOVED CORROSION & ACCOMPLISHED EA F-5330-T0309376 P1. MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 26R FROM BS 1640 - 1660 REQUIRING ADDITIONAL STRIPPING FROM BS 1620 - BS 1720. ACCOMPLISHED EA F-5330-T0309699 FUSELAGE PLATES & SKINS CORROSION LAP SEAM STRINGER 26R STATION 1621 - 1720, MAJOR REPAIR.
FORWARD PIT RT SIDEWALL FRAME INNER CHORD HAS DENT AT STATION 820 STRINGER 23R. FUSELAGE, MAINFRAME, FUSELAGE FRAME REPAIR WORK ACCOMPLISHED ON EA F-5310-T0309050 PT 1 CATEGORY B MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 20R FROM AFT EDGE OF AFT CARGO DOOR TO BS 1460 & FROM BS 1340 TO BS 1360 REQUIRING ADDITIONAL STRIPPING FROM BS 1180 TO FWD EDGE OF AFT CARGO DOOR. ACCOMPLISHED EA F-5330-T0309493 FUSELAGE PLATES & SKINS LOWER SKIN CORROSION REPAIR AT LAP JOINT STATION 1180 TO 1459 STRINGER 20R. CATEGORY A MAJOR REPAIR.
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDERLAP SEAM AT STRINGER 14R FROM BS 781 TO 800 & ON BUTT STRAP SURFACE INSIDE BUTT JOINT AT BS 781. REQUIRING ADDITIONAL STRIPPING FROM BS 781 TO 900. ACCOMPLISHED EA F-5330-T0309546 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION REPAIR AT LAP JOINT STATION 781 TO 900 STRINGER 14R. CATEGORY B MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 4R FROM BS 781 TO 900 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM & WITH CORROSION ON UPPER SKIN SURFACE. ACCOMPLISHED EA F-5330-T0309317 PART 1 ONLY. FUSELAGE PLATES AND SKIN LOWER SKIN CORROSION REPAIR AND SCRIDE LINE LRTS AT LAP JOINT STA 780 TO STA 900 S-4R. THIS IS A CLASS "A" REPAIR. MAJOR REPAIR
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDER LAP SEAM AT STRINGER 14L BS 1260 TO 1300 & FROM AFT EDGE OF L3 DOOR CUT OUT TO BS 1460 REQUIRING ADDITIONAL STRIPPING FROM BS 1180 TO 1460. ACCOMPLISHED EA F-5330 T0 309534 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION & DENT REPAIR AT LAP JOINT STATION 1180 TO 1459 STRINGER 14L CATEGORY A MAJOR REPAIR.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 4L FROM BS 781 TO 900 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM & WITH CORROSION ON UPPER SKIN SURFACE. REPAIRED IAW EA F-5330-T0309308. MAJOR REPAIR.
NUMBER 2 PYLON RT SKIN PP STATION 128 - 197 BOTTOM EDGE CORRODED. ACCOMPLISHED EA F-5450-T0308184 NACELLES / PYLON - PYLONS STRUCTURES - NR 2 STRUT RT AFT SKIN PANEL CORROSION. CATEGORY "A" MAJOR REPAIR
FRAME AT STATION 1661 STRINGER 5L. THE REINFORCEMENT ANGLE IS GOUGED REMOVED GOUGE IAW SRM 51-10-02 FOUND CHORD TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. R & R FAIL SAFE CHORD IAW SRM 51-40-02 & DWG 146N1024. MAJOR REPAIR.
CORROSION HIDDEN BETWEEN LOWER CHORD & SKIN AT PP STATION 144 - 150, LT INNER SKIN ON NR 1 PYLON. REMOVED CORROSION FROM INNER WALL OF AFT SKIN AT PP STA 144 - PP STA 150 IAW SRM 51-10-02. AFTER REWORK AREA FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FIG 101 DETAIL V ORIGINAL MATERIAL .090 MATERIAL LOSS .019 REMAINING MATERIAL .071 INSTALLED REPAIR DOUBLER IAW EA F-5450-7-T0308211 AND SB 757-54-0022 NACELLES / PYLON - PYLONS STRUCTURES NR 1 STRUT LT AFT SKIN PANEL CORROSION. CATEGORY "A" MAJOR REPAIR.
NUMBER 1 PYLON INNER WALL RT SIDE SKIN HAS SURFACE CORROSION AT PP STATION 128 - 170. ACCOMPLISHED EA F-5450-T0308247 NR 1 RT AFT SKIN PANEL CORROSION DOUBLER FABRICATED ON T14/1075862. CATEGORY "A" MAJOR REPAIR
LEFT HORIZONTAL UPPER SURFACE HAS AREAS OF EVIDENCE OF CORROSION UNDER PAINT. COMPLIED WITH STABILIZERS HORIZONTAL STABILIZER LT HORIZONTAL UPPER SURFACE SKIN REPAIR EA F-5510-T0309352 PT 1 AUG 20, 2014. MAJOR REPAIR.
FORWARD CARGO BAY RT SIDEWALL FRAME DENTED AT BS 660 BETWEEN STRINGERS 24 - 25R. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL III. REPAIRED IAW EA F-5310-T0308983. MAJOR REPAIR CAT B.
RIGHT NR 10 SLAT OUTER SKIN FROM INBD TO OTBD TE WEDGE SEVERAL PLACES HAVE SURFACE CORROSION. REPAIRED RT NR 10 SLAT OUTER SKIN IAW SRM 51-70-10 REPAIR 4 PN 114N4002-148A, SN A2-0367. FINAL DIMENSION ON DOUBLER 1, 7" X 3" 2, 9" X 3" IAW EA F-5740-T0309027 & F-5740-T0309028 WING ATTACH FITTNGS EO F-5100-7-5001 EXISTING SRM REPAIR ON NR 10 SLAT RSC TRACKING.
FOUND SCRIBE LINE IN LAP SEAM AT STRINGER 20L FROM BS 1460 TO 1620 WITH CORROSION ON TOP OF SCRIBE LINE RUNNING UNDER LAP SEAM. ACCOMPLISHED EA F-5330-T0309171 FUSELAGE PLATES & SKINS LOWER CORROSION REPAIR. THIS IS A CLASS A MAJOR REPAIR.
NUMBER 1 SLAT TE WEDGE UPPER SURFACE CORRODED AT AFT EDGE. REPAIRED NR 1 SLAT TE WEDGE UPPER SURFACE SKIN IAW SRM 51-70-10 REPAIR 4 PN 114N4002-131, SN A1-0137 FINAL DIMENSION ON DOUBLE NR 1 3" X 5.5" NR 2 6.5" X 3" #3 7" X 3". IAW EA F-5740-T0309024, F-5740-T0309025, & F-5740-T0309026 WINGS ATTACH FITTINGS EO F-5100-7-5001 EXISTING SRM REPAIR ON NR 1 SLAT RSC TRACKING.
R2 DOOR LOWER CUT OUT CREASE BEAM ANGLE CORRODED. R & R R2 DOOR INBD CHORD STATION 670 RT - 760 RT IAW SRM 51-40-02 & DWG 143N8322. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53- 30-13 FIG 10 DET VIII.
L2 DOOR CUT OUT CREASE BEAM ANGLE CORRODED AT BS 740 - 760. R & R INBD CHORD IAW SRM 51-40-02 & DWG 143N8322. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DET VI.
BS 350 FLOORBEAM UPPER SURFACE CORRODED RBL 10 TO RBL 60. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR.
BS 365 FLOORBEAM REPAIR ANGLE CORRODED, RBL 25. DUE TO NO LIMITS ON INCOMING REPAIR AT BS 365, RBL 25. FLOORBEAM INCOMING REPAIR WAS REMOVED & REPLACED AT STATION 365, RBL 25 IAW SRM 53-00-51, REPAIR NR 1, FIG 201. MAJOR REPAIR.
RIGHT INBD CREASE BEAM UPPER SURFACE CORRODED BS 395. R & R CREASE BEAM ANGLE IAW SRM 51-40-02 & DWG 141N8422. MAJOR REPAIR.
KEEL BEAM FITTING AT BS 1100 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-40-12 FIG 101 DET IV. LOCATED & DRILLED IAW SRM 51-40-05, AND INSTALLED.
MAIN CABIN AT BS 1680 RBL 9.20 DECK PLATE GOUGED. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG. 101, DETAIL III. REMOVED AND REPLACED DECK PLATE, IAW SRM 51-40-02 AND DWG 146N5318. MAJOR REPAIR.
SEAT TRACK BS 1180 - 1240 LBL 44 NICKED & GOUGEED ENTIRE LENGTH. REMOVED NICKS & GOUGES IAW SRM 53-00-52. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. R & R SEAT TRACK IAW SRM 51-40-02 & DWG 146N5123.
FLOORBEAM ATTACH STIFFENER HOLE ELONGATED AT BS 1660, BL 0. REMOVED STIFFENER IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-40-06 FIG 3 TABLE I. INSTALLED STIFFENER IAW SRM 51-40-02.
LEFT SIDEWALL FRAME HAS DENT AT STATION 1400, NEAR STRINGER 25L. EVALUATED FRAME STATION 1400, LT SIDE & DENTS NOT ALLOWED ON FLANGE IAW SRM 53-00-07, FIG 101, DETAIL II. R & R FRAME IAW SRM 51-40-02 & DWG 146N1011. FRAME WAS RECEIVED ON TRAVELER T14 1063426, STATION 1400, STRINGER 25L - STRINGER 27R. MAJOR REPAIR.
FLOORBEAM TEE BS 1640 RBL 44 - 60 CORRODED ON THE BOTTOM SIDE OF THE TOP FLANGE. REMOVED CORROSION IAW SRM 51-10-02, & FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM TEE AT BS 1640 IAW SRM 51-40-02, DWG 146N5089.
AFT CARGO BAY FRAME BS 1280, S29L - 29R GOUGED. REMOVED GOUGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 07, DETAIL II, FIG. 101. REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1005. MAJOR REPAIR.
MAIN DECK COMPARTMENT STATION 780 - 800, RT SIDE CREASE BEAM, INNER CHORD DAMAGED. REMOVED CORROSION & DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. R & R RT INBD CREASE BEAM CHORD IAW SRM 51-40-02 & DWG 143N5520, FROM BS 755 - 900. MAJOR REPAIR CAT A.
MAIN DECK BS 780 - 880 LBL 45.50 SEAT TRACK HAS CORROSION, NICKS & SCRATCHES. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101, DETAIL I. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5080. MAJOR.
DURING CLIMBOUT, 20 MINS INTO FLIGHT LEFT FORWARD BOOST PUMP CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER RESET. R & R LEFT FWD FUEL BOOST PUMP IAW AMM 28-22-03. LEAK & OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.