N924FD
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
GEAR DISAGREE MESSAGE. NLG INDICATION WAS NOT ILLUMINATED. NLG DID NOT EXTEND. COMPLETED QRH 14.1.12. AFTER CHKLST COMPLETION NLG EXTENSION SUCCESSFUL. EMERGENCY DECLARED. AFTER SHUTDOWN STATUS MESSAGE LDG GEAR MONITOR. EMERGENCY DECLARED. LANDING GEAR LOCKED DOWN. ADC VMO/MMO SWITCH SELECTED TO ALTN POSITION. PLACED ACFT TO NORMAL CONFIGURATION. CYCLED NLG MULITPLE TIMES ON JACK UNBLE TO GET NLG TO FAILED TOEXTEND. NOTICED EVERY OTHER CYCLE NLG & DOORS SLOW TO OPEN & EXTEND. SUSPECT NLG DOOR SEQUENCE VALVE, NLG DOOR ACTUATOR & NLG LOCK ACTUATOR. R & R NLG SEQUENCE VALVE, NLG DOOR ACTUATOR & NLG LOCK ACTUATOR. OPS & LEAK CHECK PASSED. CYCLED NLG MULTIPLE TIMES, ALL INDICATIONS NORMAL.
NOSE GEAR FAILED TO EXTEND NORMALLY WHEN GEAR HANDLE WAS MOVED INTO THE DOWN POSITION. NOSE GEAR EXTENDED USING THE ALTN GEAR EXTEND SWITCH. LDG GEAR MONITOR STATUS MESSAGE DISPLAYED. AMM: 32-34-05-4 COMPLETED INSTALL OF NOSE GEAR DOOR OPERATED SEQUENCE VALVE REF AMM 32-34-05-4. OPS AND LEAK CHECK GOOD. REMOVED FROM MEL CONFIG. AMM: 32-34-05-4 REMOVED AND REPLACED NOSE GEAR DOOR OPERATED SEQUENCE VALVE UP TO AND INCLUDING STEP 3. C. (7). AMM: 32-34-05-4 COMPLETED INSTALL OF NOSE GEAR DOOR OPERATED SEQUENCE VALVE REF AMM 32-34-05-4. OPS AND LEAK CHECK GOOD. REMOVED FROM MEL CONFIG.
COCKPIT EMERGENCY DOME LIGHT INOPERATIVE. RELAMPED NO HELP. DURING TROUBLESHOOTING, FOUND WIRE W0200-0009-22, BROKEN FROM RELAY R10381. RESOLDER SAME, LIGHT OPS CHECK NORMAL. DOME LIGHT ASSEMBLIES REQUIRE MOUNTING AND RE-OPS CHECK.
AFT CARGO COMPARTMENT BETWEEN BS 1440 AND 1460 LOWER SECTION BL 0.0 PROTECTIVE TREATMENT DAMAGED BARE METAL AND CORROSION EVALUATED STRINGER AT AFT CARGO BETWEEN BS 1440-1460 BL 0 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-03-1A. REMOVED STRINGER AND SPLICE BETWEEN 1433-1465 BL 0 IAW SRM 51-40-02-0G. TRIMMED, LOCATED AND DRILLED NEW STRINGER AND SPLICE IAW B757 SRM 53-00- 03-2R. INSTALLED NEW STRINGER AND SPLICE IAW B757 SRM 51-40-02-0G. BOEING DWG# PL146N3110 REV CB.
R1 DOOR FRAME BETWEEN BS 324 AND BS 333.45 TORQUE TUBE CAVITY SKIN WITH CRACK COMPLIED WITH FEDEX EA # F-5310-T0385531 P1 TITTLE: FUSELAGE - MAINFRAME - SECTION 41: STUB FRAME INSTALLATION, R1 DOOR CUTOUT, STA 335, COVER PANEL, CRACK REPAIR.
AFT CARGO COMPARTMENT BS 1560 LBL 45.50 UPPER FLOOR BEAM LOWER CHORD WITH CORROSION. COMPLIED WITH FEDEX EA # F-5310-T0385569 P1 TILE: FUSELAGE -MAINFRAME CORROSION REPAIR -STA 1560 FLOOR BEAM LOWER FLANGE DAMAGE
MAIN CARGO STA 1200 BETW BL 0 TO LBL 58 FLOOR BEAM UPPER T CHORD HAS CORROSION 7 SPOTS CUT OUT UPPER FLOOR BEAM FOUND AREA OUT OF LIMITS STA 1200 BL 0 TO LBL 58 IAW B757 SRM 53-00-51-2R FIG 201 REP 8 AND B757 SRM 53-0051-1A DET II MANUFACTURE (FORMED) REPAIR PARTS IAW B757 SRM 53-00-51-2R TABLE 202 FIG 201 DET II INSTALLED ALL REPAIR PARTS AND RE- INSTALLED PARTS WAS REMOVED FOR ACCESS IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00- 51-2R FIG 201 DET II
SKIN CRACK FOUND AT L1 OPERATING MECHANSIM CAVITY STA 327 STR 14-15 COMPLIED WITH FEDEX EA # F-5310-T0385532 P1 TITLE: FUSELAGE-MAINFRAME-SECTION 41: STUB FRAME INSTALLATION, L1 DOOR CUT OUT, STA 355, CONER PANEL, CRACK REPAIR
SLAT NR 3 UPPER SURFACE T/E HAS A SKIN DEFORMATION REPAIRED SLAT NR 3 UPPER SURFACE IAW SRM 57-43-02-1A REMOVED AND REINSTALLED SLAT NR 3 AND OPS CHECK IAW AMM 27-81-02-4, OPS CHECK SATISTFACTORY AND PERFORMED O/B SLAT LOSS SENSING TEST IAW AMM 27-81-00-5, LOSS SENSING TEST SATISFACTORY.
MAIN CARGO STA 1200 BETW BL 0 TO LBL 58 FLOOR BEAM UPPER T CHORD HAS CORROSION 7 SPOTS CUT OUT UPPER FLOOR BEAM FOUND AREA OUT OF LIMITS STA 1200 BL 0 TO LBL 58 IAW B757 SRM 53-00-51-2R FIG 201 REP 8 AND B757 SRM 53-00-51-1A DET II MANUFACTURE (FORMED) REPAIR PARTS IAW B757 SRM 53-00-51-2R TABLE 202 FIG 201 DET II INSTALLED ALL REPAIR PARTS AND RE-INSTALLED PARTS WAS REMOVED FOR ACCESS IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-51-2R FIG 201 DET II
MAIN CARGO FLOORBEAM UPPER FLANGE FOUND WITH CORROSION AT BS 1620, LBL 50. CUT OUT FLOOR BEAM SECTION FOUND AREA OUT OF LIMITS MAIN CARGO CABIN FLOORBEAM BS 1200 LBL 50 IAW SRM 53-00-21-1A DET II AND SRM 53-00-51-2R REP 8. MANAFACTURED PARTS TRIMMED, LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-40-05-0G, SRM 53-00-51-2R REP 8 TABLE 202 FIG 201 INSTALLED REPAIR PARTS IAW SRM 51-40-02-0G
MAIN CARGO BETW STA 1180 TO 1420 RBL 58 SEAT TRACK HAS CORROSION REMOVED DAMAGE SEAT TRACK. NO ALLOWABLE DAMAGE LIMITS MAIN CABIN BETWEEN STA 1180 TO 1420 RBL 58 IAW B757 SRM 51-40-02-0G AND B757 SRM 51-10-02-0G TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW B757 51-40-08-0G BOEING DWG # 657N3332 REV C INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-02-0G AND BOEING DWG# 657N3332 REV C
MAIN CARGO CABIN SEAT TRACK FOUND CORRODED AT LEVEL STA 1560 TO STA 1600 LBL 58 REMOVED AND EVALUATED MAIN CARGO CABIN SEAT TRACK BETWEEN STA 1420-1600 LBL 58 NO ALLOWABLE DAMAGE IAW B757 SRM 53-00-52-1A FIG 101, SRM51-40-02-0G. TRIMMED, LOCATED, DRILLED AND INSATLLED NEW SEAT TRACK SECTION IAW B757 SRM 51-40-05-0G,51-40-08-0G,51-40- 02-0G AND BOEING DWG # 146N5130 REV C.
MAIN CARGO BETW STA 1180-1200 LBL 45 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK SECTION BETWEEN STA 1180 TO 1240 LBL 45 FOUND SEAT TRACK OUT OF LIMITS IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-52-1A FIG 101. TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW B757 SRM 51-40-05-0G AND SRM 51-40-08-0G, BOEING DWG 146N5130 REV - DWG PL 146N5130 REV C INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40- 02-0G
MAIN CARGO BETW STA 1000-1019 LBL 24 SEAT TRACK CROWN SUPPORT HAS CORROSION. COMPILED WITH EA # F-5310-T0385669.
SEAT TRACK LBL 45.50 BETWEEN BS 1130 TO BS 1540 HAS MULTIPLE AREAS WITH CORROSION REMOVED SEAT TRACK SECTION LBL 45.5 BETWEEN STA 1320 TO 1540 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED AND DRILLED, NEW SEAT TRACK SECTIOM IAW B757 SRM 51-40-05-0G, SRM 51-40-08-0G AND BOEING DWG # 146N5130 REV C INSTALLED NEW SEAT TRACK SECTION IAW B757 SRM 51-40-02-0G
MDIS 924 33-50 2328 10FEB25 13:47 YOW FACT R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. FACT 10FEB25 14:04 YOW AMM: 33-51-06-2-1 RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE. OK TO CONTINUE.
CLIMBING THRU 12,000 FEET OUT OF BFM EICAS L EMER DOOR LIGHT. LEVELED AT 15,000 AND RAN QRH. DECLARED EMERGENCY AND DESCENDED TO 10,000 FEET. PRESSURIZATION OPERATED NORMAL AND AFTER A FEW MINUTES AT 10,000 AND EICAS MESSAGE DISAPPEARED. GAINED ACESS TO #3 EMERGENCY EXIT DOOR SENSOR AND CK'D TARGET ON SWITCH IS WITHIN LIMITS REF.M.M. 52-71-00-5 CK'D SEAL STOPS AND SEALS WERE MATING WELL ALSO CK'D PRESSURIZATION AND FOR LEAKS ALL CK GOOD AT THIS TIME REF. M.M.52-21-01-2 AND 21-31-00-5-0 OK TO CONTINUE AT THIS TIME .
ON CLIMB OUT THRU 18,000 L EMER DOOR EICAS MESSAGE. PRESSURIZATION REMAINED NORMAL CONTINUED TO DESTINATION. DESCENDING BELOW 10,000 EICS MESSAGE EXTINGUISHED. REMOVED AND REPLACED L3 DOOR LOCK PROX SENSOR REF 52-71-00-4. TESTS PASS.
REMOVE # 2 ENG PYLON I/B DRAG FITTING REQUIEST PER EA # F-5730-TO376999 REPAIR PERFORMED I.A.W EA # F-5730-TO376999 WING - OUTER WING-UPPER SKIN, DRAG FITTING AND DIAGONAL BRACE FASTENER AND SHIM INSPECTION RB 757- 57A0073. CAT "B" MAJOR REPAIR.
RIGHT WING #7 SLAT AFT SKIN HAS CRACK AROUND THE RIVET HOLE LOCATED AT INBD AUXILLARY TRACK AREA. REMOVED AND REPLACED DAMAGED SKIN ON #7 SLAT R/H WING IAW SRM 51-40-02. MAJOR REPAIR
ZONE 220 FLOOR BOARD 222AF IS DAMAGED. FABRICATED ZONE 220 FLOORBOARD 222AF ON VT MAE TRAVELER T21/1586160 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON MAE TRAVELER T21/1586166 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
ZONE 220 FLOOR BOARD 222MAF IS DAMGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1586164 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1586162 IAW SRZ-25- 005 REVISION R. MAJOR REPAIR
TE FLAP DISAGREE EICAS MESSAGE ON APPROACH. COMPLIED WITH QRH PROCEDURES, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. T/ S PER 757 F.I.M. 27-51 TREE 808. ALSO PERFORMED FSEU BITE TEST PER AMM 27-51-01-2. NO CURRENT FAULTS. OPERATED FLAPS FULL TRAVEL SEVERAL TIMES PER 757 AMM 27-50-00-5-1. NO BINDING OBSERVED EITHER AT THE FLAP HANDLE ON AT THE CONTROL MECHANISMS. NO HISTORY PAST 90 DAYS, A/C OK FOR SERVICE.
DURING ARRIVAL GOT TE FLAP ASYM WHEN FLAPS SELECTED TO 5. FLAP INDICATION SHOWS BETWEEN 1 AND 5. COMPLIED WITH QRH, LANDED UNEVENTFULLY. TRAILING EDGE FLAP INDICATION SHOWING APPROXIMATELY HALF A NEEDLE WIDTH SPLIT AFTER BLOCK-IN. LEFT AND RIGHT TRAILING EDGE FLAPS APPEAR TO BE EXTENDED SYMMETRICAL. PERFORMED FSEU BITE PROCEDURE NR 1 FSEU FAULTING MESSAGE NUMBER 314. NR 2 AND NR 3 FSEU NO FAULTS NOTED, FURTHER T/S REQUIRED, REF FIM 27-51 FT805. T/S PER FIM 27-51 TREE 809 AND TREE 805. FSEU 1 HAS 314 FAULT THAT WILL NOT CLEAR. INSPECTED TORQUE TUBES AND OVERTORQUE INDICATORS ON LT WING. NO DEFECTS AND FLAP TORQUE TUBE TURNS FREELY MANUALLY. LT FLAP POS TRANSMITTER IS 18% OFF AND ERRATIC DURING MOVEMENT. INTERNAL MOVEMENT APPEARS TO BE MESSED UP THRU SIGHT GLASS. REMOVED AND REPLACED LT FLAP TRANSMITTER. ADJ/TEST GOOD, REF M/M 27-58-03-4 AND M/M 27-58-01-5. A/C OK FOR SERVICE.
LT ELEVATOR OUTBOARD UPPER AND LOWER CONDUCTIVE FRAME ARE CORRODED. REPLACED LT ELEVATOR UPPER AND LOWER CONDUCTIVE FRAMES IAW SRM 55-20-01 AND 55-20-01-2R WITH EA F-2730-T0351345 STATIC BASE AND WICK REMOVED AND INSTALLED IAW AMM 23-61-01-2. FINISH RESTORED IAW AMM 51-20-00.
AFT CARGO FLOOR PANEL 161BF HAS 1EA PUNCTURE FABRICATED AFT CARGO FLOOR PANEL 161BF IAW B757 SRM 53-60-53 AND BOEING PL 453N1270 REV BN PARTMARKED IAW BAC5307
AFT PIT FLOOR PANEL 161AF HAS 1EA A PUNCTURE FABRICATED NEW FLOOR PANEL 161AF IAW BOEING PL 453N1270 BN-REV
LEFT WING ,OUTBOARD FLAP,AFTFLAP,INBOARD TRACK,GUIDE CRACKED. REPAIRED LEFT WING ,OUTBOARD FLAP,AFT FLAP,INBOARD TRACK,GUIDE CRACKED BY REMOVING DAMAGE AND APPLYING HOT BOND FIBERGLASS OVERLAY REPAIRS IN 2 EACH AREAS ,CURING,SHAPING AND RESTORING FINISH IAW FED EX EA# F-5750-T0351320.INSTALLED REPAIRED GUIDE IAW SRM 51 T0351320.INSTALLED REPAIRED GUIDE IAW SRM 51-40-02.
AFT MAIN CARGO FLOORBOARD P.NO 11864182-40 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2R
AFT MAIN CABIN FLOORBOARD P.NO 11864182-42 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2R
RT WING T/E WIGGLE PANEL IS CRACKED AT APPROX WSTA 335. REMOVED AND REPLACED WIGGLE PANEL AT RT WING T/E AT APPROX WSTA335 PER SRM 51-40-02-0G APPLIED PROTECTIVE FINISH PER SRM 51-20-01-0G.
ACFT ELECTRICAL SYSTEM WENT IRRADIC, COCKPIT LIGHTS BEGAN FLICKERING, LOWER EICAS WENT BLACK. NUMEROUS EICAS MESSAGES ENSUED BUT MAIN ONES REMAINED. EVERYTHING CAME BACK ON WHEN THE RIGHT ENGINE WAS SHUTDOWN. REMOVED AND REPLACED THE RIGHT ENGINE IDG IAW MM 24-11-01. LEAK AND OPS CHECK GOOD.
UPON ARRIVAL, THE L1 ENTRY DOOR EMERGENCY POWER RESERVOIR INDICATION WAS ZERO PSI. REMOVED AND REPLACED L1 ENTRY DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4. OK FOR SERVICE
STA 580 LBL 45.5 FLOORBEAM IS CRACKED. SEEN FROM FORWARD CARGO. COMPLIED WITH EA # F-5310-T0336514 P1,FUSELAGE-MAINFRAME-STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.
MAIN DECK STA 978 LT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB MAIN DECK AT STA 978 LT, ORIGINAL MAT .056", MAT REM .044" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET II FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED SHEAR WEB (CUSP WEB) IAW B DWG 144N5150 REV C REV A, INSTALLED NEW SHEAR WEB (CUSP WEB) IAW B DWG 144N5150 REV C AND REV A.
MAIN DECK BETWEEN STA 1620 - 1640 LBL 45.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK IAW B 757 SRM 51-10-02-0G,EVALUATED AREA,ORIGINAL MAT. 0.070",MAT. REMAINING 0.015",MAT. LOSS 0.055" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG 101 DETAIL VII,REMOVED SEAT TRACK SECTION STA 1540 TO STA 1640 LBL 45.5,TRIMMED,LOCATED,DRILLED AND INSTALLED NEW SEAT TRACK SECTION IAW B DWG. # 146N5130 REV - , 146N5120 REV A AND B 757 SRM 51-40-02-0G.
MAIN DECK BETWEEN STA 980 - 1000 RT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB AT STA 980 - 1000 RT, ORIGINAL MAT .056", MAT REM .048" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEW SHEAR WEB (CUSP WEB) IAW DWG 144N5150 REV A AND C. INSTALLED NEW SHEAR WEB (CUSP WEB) AT STA 980 - 1000 RT IAW DWG 144N5150 REV A REV C.
MAIN DECK BETWEEN STA 900 - 1040 LBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AND EVALUATED CREASE BEAM AT MAIN CABIN STA 900-1040 LBL 64 ORIGINAL MAT .070" MAT REMAINING .046" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLACED CREASE BEAM SECTION FROM 900 TO 1040 LBL 64 IAW B DWG 144N5152 REV -, SRM 51-40-05-0G, SRM 51-10-02-0G.
MAIN DECK BETWEEN BS 1360 - 1383, LBL 58.22 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, EVALUATED THE AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, DETAIL VII, FIG 101. REMOVED THE DAMAGED SEAT TRACK, TRIMMED, AND DRILLED A NEW SEAT TRACK SECTION.3. INSTALLED THE NEW SEAT TRACK SECTION, AND SPLICE REPAIR IAW SRM 53-00-52-2R, REPAIR 3.
MAIN DECK BS 1640 BETWEEN BL 0 - LBL 58.22 FLOORBEAM TEE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, LBL 38 TO LBL 58.22, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAL VI. CUT-OUT THE DAMAGED FLOORBEAM UPPER TEE, FABRICATED ANGLES, TEE REPAIR, TRIMMED, LOCATED, DRILLED, AND INSTALLED THE REPAIR IAW SRM 53-00-51-2R, FIG 201, REPAIR 8.
MAIN DECK STA 1110 LBL 70 CUSP WEB CORRODED. REMOVED CORROSION AT CUSP WEB MAIN DECK STA 1110 LBL 70 AND EVALUATED ORIGINAL MAT .063" MAT REM .030" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEW SHEAR WEB (CUSP WEB) IAW DWG 144N5210 REV - AND REV A. INSTALLED NEW SHEAR WEB (CUSP WEB) IAW DWG 144N5210 REV - AND REV A.
MAIN DECK BETWEEN STA 900-1040 RBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN CREASE BEAM STA 900 AT 1040 RBL 64 AND FOUND TO BE OUT OF LIMITS ORIGINAL MAT .070" MATERIAL REM . 050" IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLACED CREASE BEAM SECTION FROM 900 TO 1040 RBL 64 IAW DWG 144N5152 REV - AND SRM 51-40-05-0G, 51-10-02-0G.
MAIN DECK WEB BETWEEN BS 1640 - 1680, LBL 54 CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02-0G, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A, DETAIL VIII, FIG 101. REMOVED THE WEB, FABRICATED AND INSTALLED A NEW WEB IAW DWG 657N4304, REV - AND SRM 51-40-02-0G.
MAIN DECK BETWEEN BS 1370 - 1415, LBL 64 CREASE BEAM CORRODED. D. REMOVED THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-60-13-1A, DET II AND III, CUT OUT DAMAGE SECTION FROM BS 1480 TO 1360 IAW SRM 53-00-13-2R. LOCATED AND DRILLED A NEW CREASE BEAM, CHANNEL, AND STRAP IAW SRM 53-00-13-2R, DETAIL I, FIG 201. INSTALLED THE NEW CREASE BEAM SECTION AND REPAIR PARTS IAW SRM 53-00-13-2R, DETAIL I, FIG 201.
MAIN DECK CREASE BEAM BETWEEN BS 1610 - 1620, LBL 64 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A, DET II. CUT OUT THE DAMAGE AREA BS 1570 TO 1630 IAW SRM 53-00-13-2R, LOCATED, DRILLED, AND TRIMMED A NEW CREASE BEAM SECTION, REPAIR CHANNEL AND STRAP. INSTALLED THE CREASE BEAM SECTION AND REPAIR IAW SRM 53-00-13-2R, DET 1, FIG 101.
CORROSION BS 1434 STR 26L STRINGER AT AFT CARGO PIT. REMOVED DAMAGED ON STRINGER 26L STA 1434,EVAL ORINAL MAT. 0.080",MAT. LOSS 0.080",MAT. REMAINING 0.000",FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-03-1A FIG 101,DETAIL II AND B DWG. # 140N1530 REV. A,CUT-OUT DAMAGED,FABRICATED STRINGER AND SPLICE REPAIR,TRIMMED,LOCATED AND INSTALLED STRINGER 26L REPAIR IAW B 757 SRM 53- 60-03-01 FIG. 1 DETAIL I AND 53-00-03-2R FIG 201,REPAIR 2.
L1 DOOR IS HARD TO OPEN AND CLOSE. LUBRICATED THE DOOR IAW MM 12-21-18-3. OPERATED THE DOOR IAW MM 52-11-00-2. OPS CHECKED NORMAL. OK FOR SERVICE.
L1 DOOR SLIDE LIGHT. R & R THE BULB, LIGHT OPS NORMAL
FORWARD CARGO COMPARTMENT DOOR AFT UPPER CORNER OF DOOR STRUCTURE, ONE EACH BRACKET IS CRACKED. REMOVED, HFEC BRACKET, FOUND TO BE CRACKED. FABRICATED NEW BRACKET & INSTALLED NEW BRACKET IAW SRM 51-40-02, NDTM PT6 51-00-19 & DWG 69-53919 REV B & C.
FL390, STARTED TO OBSERVE DELAMINATION IN CAPTAIN`S FWD WINDSHIELD, FOLLOWED IMMEDIATELY BY WINDSHIELD SHATTER. R & R L1 WINDOW ASSEMBLY IAW AMM 56-11-01-4.
DURING SERVICE CHECK & OPS CHECK OF EMER EXIT LIGHTS, UPON ACTUATION OF SWITCH, NOTICED HALF OF UNARMED LIGHT WOULD FLICKER. UPON TRYING TO DISASSEMBLE TO RE-LAMP, LOWER HALF OF LIGHT ASSEMBLY BASICALLY CRUMBLED IN MY HAND. REPLACED EMER LIGHT UNARMED LEN & DRAWER ASSEMBLY. OPERATIONS CHECKED NORMAL.
DURING SERVICE CHECK & OPS CHECK OF EMERGENCY LIGHTS, ON ACTUATION OF SWITCH, NOTICED HALF OF UNARMED LIGHTS WOULD FLICKER. TRIED TO DISASSEMBLE TO REPLACED THE LAMPS, LOWER HALF OF LIGHT ASSEMBLY BASICALLY CRUMBLED. REPLACED EMERGENCY LIGHT "UNARMED" LENS AND DRAWER ASSEMBLY PER SWPM, OPS CHECKED NORMAL.
FWD M.E.C. CUT OUT FRAME BS 231 ON FWD SIDE IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW EA F-5310-T0303943 P1.
THE LT FWD WINDOW STARTED ARCHING IN FLIGHT. TURNED WINDOW HEAT OFF IAW THE QRH. WINDOW SHATTERED ABOUT FIVE MINUTES LATER. REMOVED AND INSTALLED NEW L1 WINDOW IAW MM 56-11-01-4 .
WHEN THE LT DOOR OPENED THE SLIDE FELL OUT OF THE BOX. INSTALLED L1 DOOR SLIDE USING AMM 25-66-01-4. COVER INSTALLED. OPS CHECKED GOOD.
DURING DESCENT, RECEIVED MOMENTARY "GEAR NOT DOWN" EICAS WARNING. ALTITUDE WAS APPROX 30,000 FT WARNING ONLY APPEARED ONE TIME AND LASTED ONLY A FEW SECONDS. NO EICAS FAULTS ON GROUND AND PILOT STATED THAT FAULTS WERE MOMENTARY IN FLIGHT. R & R PSEU REF 32-09-04-4 AS PRECAUTIONARY MEASURE. ALL OPS CHECKED GOOD.
AFTER NORMAL LANDING, RECEIVED NUMEROUS EICAS ALERTS THAT CLEARED BEFORE THEY COULD BE READ, BELIEVE THEY WERE DOOR RELATED. ESTIMATE IT WAS SIX ALERTS, NO CURRENT FAULTS AND PILOT STATED THAT FAULTS WERE MOMENTARY. R & R PSEU REF AMM 32-09-04-4 AS PRECAUTIONARY MEASURE. ALL OPS CHECKS.
DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.
UPON REACHING CRUISE ALITIUDE OF FL 400, BOTH THE LT & RT MAIN FUEL TANK QUANT INDICATORS WENT BLANK AND RECEIVED "FUEL QUAN IND" STATUS MSG. AFTER REACHING 4000' BOTH INDICATION CAME BACK ON WHILE FLYING APPROACH. PERFORMED THE WALK THROUGH FIM 28-41-00 TREE 857 AND NO DEFECT NOTED. PERFORMED A FUEL QUANTITY BITE PROCEDURE IAW AMM 28-41-00-5-2. NO HISTORY NOTED, AND NO CURRENT FAULTS NOTED. INSTALLED FUEL QUANTITY PROCESSOR IAW AMM 28-41-08-4, PERFORMED OPERATIONAL TEST- FUEL QUANTITY INDICATING SYSTEM IAW AMM 28-41-00-5-2. OPS TESTED GOOD, NO DEFECT NOTED. THE FUEL QUANTITY PROCESSOR RACK, PINS AND PLUG HAS BEEN INSPECTED FOR ANY DAMAGE AND SECURITY, NO DAMAGE NOTED. ACFT OK FOR SERVICE.
SKIN DAMAGE BS 1695 S19R. CUT OUT DAMAGED AREA IAW SRM 51-10-02 AND EA F-5330-143903. FABRICATED REPAIR DOUBLER AND FILLER IAW EA F-5330-143903 AND SRM 53-00-01 REPAIR 15. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 REPAIR 15 AND EA F-5330-143903.
CAPT SLIDING WINDOW LOCK VERY DIFFICULT TO MOVE AND HAND CRANK AND OVER CENTER LOCK MOVE TOWARD OPEN WHEN CRANK HANDLE RELEASED. RIGGED CLUTCH MECH, AND COMPLETED ADJ AND TEST.
L1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE FROM INSIDE. HANDLE IS LOOSE. RESECURED L1 DOOR HANDLE AS REQ'D. L1 DOOR CHECKS GOOD IAW AMM 52-11-00-6 NR 1,2 AND 4 PASSENGER DOORS - INSPECTION/CHECK. ACFT OK FOR SERVICE.
EXISTING FRAME REPAIR AT STA 1460 IS IAW SRM 51-70-11, FIG 1. REPAIR AND FOUND REPAIR WAS NOT COMPLIANT WITH SRM SPECIFIC REPAIR. REMOVED EXISTING IAW SRM 51-40-02. FABED REPAIR SPLICE ON STAM TRAVELER T10/844785. REPAIRED FRAME AT STA 1460 BETWEEN S-25L TO S-27L IAW SRM 53-00-07 FIG 201 REPAIR 5. THIS IS A CATEGORY "B" REPAIR WITH SUPPLEMENTAL INSPECTION DATA. DO A HFEC AND DETAILED INSPECTION AT 27,000FC AFTER REPAIR INSTALLATION OR 50,000FC WHICHEVER COMES FIRST. THERE AFTER DO AN HFEC INSPECTION AND DETAILED EVERY 12,000FC INTERVAL.
ENLOGATED HOLES FOUND IN INCOMING SKIN ALONG STR 26L LAP SPLICE STA 520-640 COMPLY WITH ATTACHMENT "B" OF E.O. F-5100-7-5001 PT 1. REF E.A. F-5330-131197 FOR FOLLOW-UP TRACKING REQUIREMENTS, AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.
FASTENER HOLE CRACKED IN 143N1025-12, FRAME AT STA 540 BETWEEN STR 25L-26L. COMPLY WITH ATTACHMENT "B" OF EO. F-5100-7-5001 PT. REF EA F-5310-139163 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.
SHORT EDGE MARGIN CONDITION IN INBD CHORD AT STA 460, STR. 23L COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1, REF EA F-5310-139164 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.
POTENCIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-21 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640 STR 17R TO 18R , COMPLY WITH ATTACHMENT "B" OF EO F-5100-705001 PT 1. REF EA F-5310-139165 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.
GOUGE DAMAGE ON DSS UPPER SILL SKIN AND MCD EXTERNAL SKIN BETWEEN STA 500-515 AND 580-600 NEAR STR 3L COMPLY WITH ATTACHMENT "B" OF SO F-5100-7-5001 PT 1 REF EA F-5330-139162 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.
FUS SKIN DENTED APPROX STA 1635 2" ABOVE STR 24R EVALUATED DENT AT STA 1635 2" ABOVE S-24R A=1.0 Y=.040 A/Y RATION=40. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201, REPAIR 3 CATEGORY "B" REPAIR WITH SUPPLEMENTAL INSP THRESHOLD OF 25,000 FC WITH REPEAT INSP OF 6,000 FC IAW SRM 53-00-01, FIG 201, REPAIR 3 NOTES H,I, AND TABLE V.
STA 1676 3" INBD OF STR. 28R FUSE SKIN DENTED. CHECK DENT LIMITS FOUND TO BE OUT OF LIMITS, DEPTH "Y" .131 MAX ALLOWABLE IS .125 IAW SRM 53-00-01 DETAIL 3, REPAIRED DENT DAMAGE IAW SRM 53-00-01 FIG 201, REPAIR 7, THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECTED AT 24,000 FLT CYCLES AND 12,000 FLT CYCLES THERE AFTER.HFEC INSPECT IAW NDT MANUAL PART 6 51-00-01. THIS IS A MAJOR REPAIR.
NR 3 SLAT HAS CORROSION BETWEEN UPPER SKIN ASSY & LOWER SKIN IN SEAM AREA. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.5,W=1.0,D=.01 ORIG. MAT.063. REMAINING .053 OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DET III. ACCOMPLISHED EA 5740-139134,WINGS L/E DEVICES NR 3 ALT COVE ANGLE SPLICE REPAIR OSS 518.5, P/N 114N4004-7 COVE ANGLE. SLAT PN 114N4004-175A, SN A1-0619. MAJOR REPAIR.
DENT AT STA 1704 BETWEEN S-15L TO S16L. ACCOMPLISHED EA F-5330-131187. FUSELAGE PLATES/ SKIN DAMAGE TO AND NEAR EXISTING REPAIR BS 1701, BETWEEN S-14L AND 16L. THIS IS A CLASS "B" REPAIR, PRIOR TO ACFT REACHING 37,500 FC NEW 8100-9 WILL NEED TO BE ISSUED. MAJOR REPAIR.
VENT/COOLING FAN AT STA 1681 STGR 28L INTERFERES WITH INSTALLATION OF THE E-7 RACK. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD. A REPAIR WAS ACCOMPLISHED AT STA 1678 STGR 26L-28L ON MAE EA 757-5362-16-F2577 REV-, MAE MOD W/C 118550428ACSR01. THIS N/R IS FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.
PREVIOUS REPAIR AT BS1681-8, FLOORBEAM LBL 24.75 TO 32.5 HAS CORROSION ON UPPER FLANGE. PREVIOUS BLEND OUT AT LBL 32.5 IS PITTED. REMOVED EXISTING REPAIR IAW EA NR F5310-131583, FABRICATED REPAIR STRAP FROM MAT 7075-76 0.090", FABRICATED REPAIR ANGLE NR 1, NR 2 ON FAB. SHOP (MAE) TRAVELER NR T10824094 AND NR T10874055, LOCATED AND DRILLED AND INSTALLED REPAIR STRAP , ANGLES REPAIR NR 1, NR 2 IAW EA NR F5310-131583. FUSELAGE CORROSION AT EXISTING BS 1681 FL BEAM REPAIR, AT LBL32.5. MAJOR REPAIR.
NR 7 SLAT HAS CORROSION IN SKIN SEAM BETWEEN UPPER NOSE SKIN ASSY & LOWER AFT EDGE ASSY. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA, L=10.25 ,W=.75, D=.018, ORIG MAT.063 REMAINING .045 OUT OF LIMITS IAW SRM 57-43 -01, FIG 101 DET III. ACCOMPLISHED EA F-5740-139135. WINGS L/E DEVICES- NR-7 SLAT COVE ANGLE SPLICE REPAIR, PN 114N4002-8, SLAT PN 114N4005-184A, SN A2-0613. MAJOR REPAIR.
NR 6 SLAT HAS CORROSION IN SEAM BETWEEN NOSE UPPER SKIN ASSY AND LOWER AFT EDGE SKIN. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02 FIG 101, DET II. REMOVED COVE ANGLE IAW 51-40-02 INSTALLED COVE ANGLE & REPAIR SPLICE IAW SRM 51-40-02 & SRM 51-70-11 FROM OSS 106.0 - OSS 272.62 ON SLAT NR 6. MAJOR REPAIR.
NR 10 SLAT HAS CORROSION IS SEAM BETWEEN UPPER NOSE WEDGE SKIN & AFT EDGE SKIN ASSY. REMOVED CORROSION ON NR 10 SLAT COVE ANGLE IAW SRM 51-10-02 BLEND OUT DIM L 131" ,W 1.0", D.20". FOUND OUT OF LIMITS IAW SRM 57-43-02 FIG 10, DET 2 COMPLIED WITH EA NR F-5740-131183 ON NR10 SLAT COVE ANGLE SPLICE REPAIR OSS 736.70 - 768.0, PN 114N4002-8. THIS IS A MAJOR REPAIR.
3EA FASTENER HOLES MIS- LOCATED IN THE INBD SKIN PANEL ASSY, PN 311N5046Y54, COMMON TO THE INBD 311N5220-52, BATHTUB FITTING AND 1EA C/M TO THE PN 311N5220-54, MID-CHORD. REMOVED DAMAGE FROM HOLES "B" AND "C" TO SIZE .408, AND HOLE "A" TO SIZE .567, AND PERFORMED HFEC IAW EA 757-5400-16-F2559, NO CRACKS NOTED. FABRICATED FREEZE PLUGS IAW TRAVELER NR T10/821960, AND T10/821991- AND SRM 51-20-07. INSTALLED FREEZE PLUGS (3) EACH IAW EA 757-5400-16-F2559, AND SRM 51-20-07. TREATED AND PRIMED IAW SRM 51-20-01. COMPLIED WITH EA F-5400-131592, "NACELLES / PYLONS- AD 2004-12-07/ EO F-5450-7-5003, 1 PYLON INBD SKIN MIS- DRILLED HOLES. (PYLON STA 185- 206). MAJOR REPAIR.
NR 5 SLAT HAS CORROSION ON LOWER NOSE SKIN AND UPPER SKIN BUTT UNDER SEALANT. REMOVED CORROSION FROM COVE ANGLES AND SPLICE IAW SRM 51-10-02 ORIGINAL MATERIAL .080 AFTER REWORK .060 MATERIAL LOSS .020 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101. FABRICATED NEW ANGLES AND SPLICES ON TRAVELERS NR 10/829393,T10/829394,T10/829395 &T10/829387 AND INSTALLED NEW ANGLES AND SPLICES IAW SRM 51-40-02. MAJOR REPAIR.
AT STA 640 AND 780 THERE IS A MISMATCH IN HEIGHT BETWEEN THE SEAT TRACK CROWNS THAT WILL PREVENT THE HANDLING SYS ROLLER TRAYS FROM SITTING LEVEL. RBL 24-75 AND 45.5. THIS IS AN EXISTING CONDITION. DUE TO DISCREPANCY EFFECTING THE PTF MOD A REPAIR HAS BEEN ACCOMPLISHED AT STA 640-780 RBL 24.75 AND 45.5 IAW MAE EA 757-5335-16-F2562 REV B AND MAE 43435600001. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
RT WING FIXED L/E,THROUGH ACCESS HOLES, BEHIND NR 10 SLAT, CORROSION ON INNER SURFACE. REMOVED CORROSION RT WING FIXED L/E AT ANGLE IAW SRM 51-10-02, BLENDED AREA L=5.0", W=1.0", D=0.050", MAT ORIG. .050", OUT OF LIMITS IAW SRM 57-41-13, FIG 101 DET II. R & R NEW ANGLE IAW SRM 51-40-02. MAJOR REPAIR.
LT WING NR 1 SLAT LOWER COVE APPROX 10" OTBD OF NR 1 SLAT TRACK ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=40",W= 1.0,D=.040, ORIG MAT REMAINING .023 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET III. ACCOMPLISHED EA F-57-40-131184. WINGS L/E DEVICES NR 1 SLAT COVE ANGLE SPLICE REPAIR OSS768.0. PN114N4002-8 COVE ANGLE, SLAT ASSY 114N4002-154A, SN A2-0619. MAJOR REPAIR.
STR 25L AT STA 1650 HAD DEFORMED HOLE. R & R STRINGER AT STA 1650 S-25L IAW SRM 53-00-03 FIG 201, REPAIR 1 DETAIL II. FOUND HOLE TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
CORROSION LOWER SURFACE OF LOWER SILL AT DOOR L-3 ON ACFT. R & R L-3 DOOR LOWER SILL WEB FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101 DETAIL III AND SRM 51-40-02. CLASSIFIED MAJOR REPAIR.
LT WING MLG TRUNNION FAIRING FWD ATTACH POINT SKIN IS CORRODED UNDER AND AROUND MOUNT REPAIRED LT WING LOWER SKIN AT MLG FAIRING FWD ATTACH POINT 7 IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
RT WING MLG TRUNNION FAIRING FWD MOUNT AREA WING LOWER SKIN HAS CORROSION REPAIRED RT WING MLG TRUNNION FWD ATTACH POINT IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
LT WING NR 5 SLAT T/E WEDGE INNER SURFACE ABOVE INBD AUX TRACK IS DELAMINATED. REMOVED DAMAGE AND BONDED REPAIR SKIN AND DOUBLER ON LT WING NR 5 SLAT T/E WEDGE IAW SRM 51-70-10. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
LT WING NR 2 SLAT COVE ANGLE CORRODED.
RT WING AT NR 2 PYLON MOUNT AREA INBD STRUT MOUNT FITTING, BUSHING HAS SCRATCH AND WEAR MARKS. ACCOMPLISHED OVER SIZED LUG HOLE REPAIR IAW FINAL EA NR F-5720-131160, WINGS- FITTINGS-(AD 2004-12-07) NR 2 ENG PYLON INBD SIDE LOAD FITTING BUSHING O/S HOLE AND FAA FORM 8100-9 ATTACHED, THIS A MAJOR REPAIR.
RT WING NR 2 PYLON MOUNTING AREA OTBD STRUT MOUNT FITTING HAS GOUGES ON 2 PLACES AT INNER AND OUTER SURFACE. ACCOMPLISHED FINAL EA F-5740-131580, WINGS-(AD 2004-12-7/EO F-5450-7-5003) RT OTBD SIDE LOAD FITTING GOUGED THIS IS MAJOR REPAIR.
UNABLE TO INSTALL IEA FASTENER IAW EO F-5450-7-5003C PT3 & PT4, FOR THE LT & RT WING ISLF. INSTALLED 2EA BACB30US10K BOLTS IAW EA F-5450-131166 IN THE LT & RT WING ISLF. FAA FORM 8100-9 ATTACHED. ( LOCATION PP-RBL 9, WS 285.65 ). MAJOR REPAIR.
SEAT TRACK AT LBL 45.5 STA 1160 AND 1139 HAS MINOR NICK DAMAGE AT TOP OF CROWN. CHECK LIMITS AT STA 1160 DIMENSION ARE 1.0 X 0,6 X 0.030, AT STA 1139 DIMENSIONS ARE 1.0 X 0.6 X0.025 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I PG 102. FABED NEW SEAT TRACK IAW DWG 144 N5021 SEAT TRACK IS R & R IAW PTF MOD FROM STA 1080 TO 1180, LBL 45.5. THIS IS A CLASSIFIED AS A MAJOR REPAIR.
MAIN CABIN STA 1360-1380 LT SIDE CREASE BEAM WEB HAS CORROSION R & R LT SIDE CREASE BEAM WEB FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL II AND SRM 51-40-02. FABRICATED NEW CREASE BEAM WEB ON MAE TRAVELER NR T10/818082. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN SEAT TRACK STA 780-900 RBL 25 IS GOUGED AND HAS CORROSION R & R SEAT TRACK AT STA 780-879 RBL 25 FOUND OUT OF LIMITS IAW SRM 51-30-02, FIG 101 DETAIL I AND SRM 51-40-02. SEAT TRACK FABRICATED ON MAE TRAVELER NR T10/817651. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION STA 1180 TO 1200 LT SIDE. REMOVED AND REPLACED LT SIDE IB CREASE BEAM AT STA 1180-1280, FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN STA 620-640 RT SIDE CREASE BEAM WEB HAS CORROSION. R & R RT SIDE CREASE BEAM WEB. FOUND OUT OF LIMITS IAW SRM 53-13-30, FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 560-580 RT SIDE CREASE BEAM WEB HAS CORROSION AT SCREW HOLE ON UNDERNEATH SIDE. R & R RT SIDE CREASE BEAM WEB, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 1020-1040 RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED AND REPLACED RT SIDE CREASE BEAM WEB STA 1020-1040, FOUND OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DETAIL III AND SRM 51-40-02. WEB FABRICATED ON MAE TRAVELER T10/821027. CLASSIFIED CATEGORY "A" MAJOR REPAIR
APU INLET DUCT CUTOUT INNER AREA FWD, AFT FRAMES NUT PLATES CORRODED. REMOVED DAMAGE IAW SRM 51-10-02, AND CORROSION IAW SRM 53-80-01 PG 106 FIG. 101. DETAIL 5, FOUND OUT OF LIMITS FABED, NEW STRAP ON TRAV NR T10/820801, INSTALLED AT STA 1786 STR 3R-6R IAW SRM 51-40-02 , ( AFT STRAP REPLACED ON NR N01046, WO:00046433)THIS IS CATEGORY A, MAJOR REPAIR.
APU INLET AFT STRAP STA 1825 CORRODED AT STR 3R -6R. REMOVED AND REPLACED APU INLET AFT STRAP AT STA 1825 BETWEEN STRINGER 3R-6R IAW SRM 51-40-02, PART FABED ON TRAV NR T10/822996, MAJOR REPAIR.
NR 8 SLAT L/E UPPER FACE CTR SECTION HAS CRACK REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.5" W=1.2" D=.023 ORIG. MAT .063 OUT OF LIMITS IAW SRM 57-43-01 FIG 101, DET VII. REPAIRED IAW SRM 57-43-01 FIG 201 R NR 1 & EA F-5740-131175. WINGS- L/E DEVICES, SLAT NR 8 MINOR DEVIATION TO SRM REPAIR, "SLAT ASSY, PART NR 114N004-176, SN A2-0618", MAJOR REPAIR.
NR 2 SLAT ASSY LOWER FACE T/E OF LOWER AREA SKIN IS CORRODED.
DENT ON EXTERNAL FUSELAGE SKIN BS 562 S-29R. SDR ENTERED IN ERROR. NO DENT AT THIS LOCATION.
NR 2 PYLON TORQUE BOX ASSY RT AND LT SIDE INNER SKIN SURFACE HAVE CORROSION RUNING DOWN THE LOWER CHORD. INSTALLED NEW SKIN PN 311N5046Y53, IAW SRM 51-40-02, DWG 311N5002, AND EO F-5450-7-5003, P5, CORROSION ON SKIN BLENDED OUT OF LIMITS PER SRM 54-40-02. REPLACED SKIN IAW SRM 51-40-02 REPAIR IS CLASSIFIED AS MAJOR REPAIR.
LT WING OTBD FLAP L/E APPROX 24" FROM OTBD EDGE IS DENTED. EVALUATED DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01 FIG 101. REPAIRED LT WING OB FLAP L/E IAW SRM 57-53-01, FIG 201 REPAIR NR 2.
SKIN DENT AT BS 755 BETWEEN S-17L TO S-18L. DENT WAS FOUND TO BE WITHIN LIMITS. NO MX ACTION REQUIRED.
NR 1 PYLON RT INNER SKIN HAS CORROSION RUNNING INTO SPLICE, ACCESS THRU PANEL 433HR AND 433JR. CORROSION ON SKIN BLENDED OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL II. REPLACED SKIN ASSY WITH PN 311N5046Y54, SKIN PANEL ON SERVICABLE PARTS TAG NR 1455B2 IAW SRM 51-40-02, AND DWG 311N5002, REPAIR IS CLASSIFIED AS MAJOR REPAIR.
MAIN CABIN FLOORBEAM STA 720 LBL 62 HAS CORROSION AT SCREW HOLE. REMOVED CORROSION IAW 51-10-02. ORIG MAT .125" AFTER REWORK .080 OUT OF LIMITS IAW SRM 53-00-51, FIG 1, DET III, REPAIRED IAW SRM 53-00-51 FIG 201 R1, THIS IS CAT. "A" REPAIR. MAJOR REPAIR.
RT WING SLAT NR 6 L/E SKIN HAS A DENT WS-179.
DENT AT FUSELAGE SKIN BS 1665 S-29L. UPON FURTHER INSP, FOUND DAMAGE TO HAVE BEEN CAUSED BY A LIGHTNING STRIKE. REPAIRED DAMAGE IAW SRM 53-00-01-201 REPAIR 6. CLASSIFIED MINOR REPAIR.
MAIN CABIN STA 365-377 RT SIDE CREASE BEAM WEB CORRODED ON UNDERNEATH SIDE BLENDED CORROSION & FOUND TO MEASURE OUT OF LIMITS IAW SRM 53-30-13, FIG 101 DETIAL II. R & R WEB IAW SRM 51-40-02. FABRICATED NEW WEB IAW DWG 141N8422. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN SEAT TRACK STA 418-440 RBL 25 IS GOUGED AND HAS CORROSION. REMOVED AND REPLACED SEAT TRACK MEASURED OUT OF LIMITS. IAW SRM 51-40-02 AND SRM 53-00-52 FIG 101 DETAIL IV. FABRICATED SEAT TRACK FROM MAT BAC1520-792 BATCH NR 0001571736. IAW SRM 53-10-52. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 740-760 RT SIDE CREASE BEAM WEB HAS CORROSION. R & R CREASE BEAM, MEASURED OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL II AND SRM 51-40-02. FABRICATED NEW WEB IAW DWG 143N8322-29. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN SEAT TRACK STA 418-440 RBL 45 IS GOUGED AND HAS CORROSION. REMOVED AND REPLACED SEAT TRACK MEASURED OUT OF LIMITS IAW SRM 51-40-02 AND 53-00-52 FIG 101 DETAIL IV. FABRICATED SEAT TRACK FROM MAT BAC1520-792. BATCH NR 0001571736 IAW SRM 53-10-52. CLASSIFED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 660-680 RT SIDE INBD CREASE BEAM CHORD HAS CORROSION. R & R RT SIDE IB CREASE BEAM CHORD AT STA 660-760 FOUND OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 395-418 RT SIDE IB CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. CREASE BEAM FOUND TO BE OUT OF LIMIT IAW SRM 53-30-13 FIG 101 DETAIL III. INSTALLED NEW CREASE BEAM AT STA 295- 418 RT IAW SRM 51-40-02. MAJOR REPAIR.
MAIN CABIN RT CREASE BEAM STA 295-377 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CREASE BEAM FOUND TO BE OUT OF LIMIT IAW SRM 53-10-15 FIG 101 DETAIL III. L=.075, W=.075, D=.022. INSTALLED NEW CRASE BEAM IAW SRM 51-40-02, AT STA 295- 377 RT. MAJOR REPAIR.
FLOORBEAM AT STA 377 LBL-47 HAS DEEP SCRATCH ON UPPER FLANGE. R & R UPPER T-CHORD MEASURED OUT OF LIMITS IAW SRM 53-00-51, FIG 201 REPAIR 3 AND SRM 53-00-01 FIG 101 DETAIL III. FABRICATED REPAIRS ON MAE TRAVELER NR T10/819048, T10/819047. CLASSIFIED CATEGORY :"A" MAJOR REPAIR
SEAT TRACK LBL 24 GOUGED FROM STA 680-780.
LT WING NR 1 SLAT IB OF PANEL 525CB INNER COVE PANEL CRACKED. REMOVED COVE PANEL IAW SRM 51-40-02, FABRICATED COVE PANEL ON TRAVELER T10/828657. LOCATED & DRILLED PANEL IAW SRM 51-40-05 TREATED & PRIMED IAW SRM 51-20-01. INSTALLED COVED PANEL TO NR 1 SLAT IAW SRM 51-40-02. MAJOR REPAIR.
LT WING NR 3 SLAT OB SIDE OF INNER COVE PANEL WITH PANEL 523BB ATTACHED IS CRACKED. REMOVED SEAL RETAINER &GUSSET FOR ACCESS, REMOVED COVE PNL IAW SRM 51-40-02. UPON REMOVAL FOUND GUSSET GOUGED, BLENDED GOUGE ON GUSSET, IAW SRM 51-10-02 ORIG MAT'L .032", MAT'L AFTER REWORK .020" FOUND OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DET IV, FABRICATED GUSSET MAT'L USE 7075-T6-.032C" BATCH 31672485, FABRICATED COVE PNL IAW SAMPLE, ORIGINAL MAT'L 7075-T6-.56C" BATCH 1512018, SUBSTITUTE MAT'L USED IAW, SRM51-30-01 TREATED & PRIMED ALL PARTS IAW SRM 51-20-01, INSTALLED ON NR N01116. MAJOR REPAIR.
LT WING NR 4 SLAT OTBD LOWER SURFACE AFT OF ANTI ICE COVE PANEL CORRODED. ACCOMPLISHED EA F5740-131579. WING LT NR4 SLAT SKIN CORROSION. MAJOR REPAIR.
MAIN CABIN STA 1440-1460 RT SIDE CREASE BEAM WEB HAS CORROSION. R & R RT SIDE CREASE BEAM WEB AT STA 1440-1460. FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL III AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
AFT CARGO COMPT- MAIN CARGO DECK FLOOR WEB LOWER SURFACE HAS CORROSION BETWEEN BS 1699-1704 LBL 23.
STA 365-418 RBL 24 SEAT TRACK SUPPORT IS CORRODED ON FWD END ( STA 365). R & R SEAT TRACK SUPPORT, MEASURED OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL VII AND SRM 51-40-02. FABRICATED NEW SUPPORT ON MAE TRAVELER NR T10-819045. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
STA 365-418 RBL 45 SEAT TRACK SUPPORT CORRODED FWD END (STA 365). R & R SUPPORT & FOUND OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DETAIL VII AND SRM 51-40-02. FABRICATED SUPPORT ON MAE TRAVELER NR T10/818708. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA 1380-1400 RT SIDE CREASE BEAM WEB HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 51-40-02 AND SRM 53-60-13 FIG 101 DETAIL III. FABRICATED NEW WEB ON MAE TRAVELER NR T10/819633. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN STA 1400-1420 RT SIDE CREASE BEAM WEB HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 51-40-02 AND SRM 53-60-13 FIG 101 DETAIL III. FABRICATED NEW WEB ON MAE TRAVELER NR T10/819634. CLASSIFIED CATEGORY "A" MAJOR REPAIR
MAIN CABIN STA 1420-1440 RT SIDE CREASE BEAM WEB HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 51-40-02 AND 53-00-13 FIG 101 DETAIL III. FABRICATED NEW WEB ON MAE TRAVELER NR T10/819635. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
FLOORBEAM AT STA 1640 REQUIRES REPLACEMENT. DUE TO EXISTING REPAIRS R & R A NEW FLOORBEAM, FABBED WITH MAT PN BAC1518-338 BATCH NR 0001773774 AND DWG 146N5089 AT STA 1640 RBL-60 TO LBL-60 IAW SRM 51-40-02. THIS IS A MAJOR REPAIR.
FLOORBEAM AT STA 1661 REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. R & R FLOORBEAM AT STA 1661 FROM LBL 68 TO RBL 68 IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
MAIN CABIN FLOORBEAM STA 365 RBL 48 IS GOUGED. REMOVED GOUGED AREA STA 365, RBL 47, ORIG MAT .125, MATERIAL REMOVED .014. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED AND FABRICATED NEW UPPER TEE CHORD IAW SRM 53-00-51, FIG 201, REPAIR 3, RECEIVED -2 AND -3 REPAIR ANGLES ON MAE FAB TRAV NR T10/817732, -4 AND -5 REPAIR STRAPS ON MAE FAB TRAV T10/817733. INSTALLED UPPER TEE CHORD AND REPAIR ANGLES AND STRAPS AT 365, RBL 70 TO LBL 14 IAW SRM 53-00-51, FIG 201, REPAIR 3. THIS IS A CAT "A" MAJOR REPAIR.
DEEP GOUGES IN FRAME 1280 BETWEEN S-10R AND S-14R MAIN CARGO DECK. REMOVED GOUGES IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DET II. REPAIRED FRAME AT BS 1280, S10-14R, IAW SRM 53-00-07, FIG 201, R1. THIS IS A CLASS "B" REPAIR WITH SUPPLEMENTAL INSPECTIONS EVERY 12,000 F.C. 'S, PER TABLE 203PG-207 OF SRM 53-00-07, FIG 201, RI. NOTE: REFERENCE ER 10-00343 FOR DISPOSITION. MAJOR REPAIR.