N979FD
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
DURING CURRENT DROP-IN VISIT IN IND, THE FLOOR BEAM SEGMENT AT STA 580 AND LBL 45 WAS FOUND CRACKED UNDER THE LBL 45 SEAT TRACK. CREATED EA E.A.#: F-5310-T0387857 TITLE: FUSELAGE - MAINFRAME - STA 580 AND LBL 45 STUB FLOOR BEAM CRACKED REPAIR PER DRAWING SR57-53-004 (FORM 8110-3 APPROVAL ATTACHED) - TRACKING EA PART 1 PROVIDES DOCUMENTATION OF THE REPAIR BEING PERFORMED PER FEDEX DRAWING SR57-53-004. PART 2 PROVIDES INSPECTIONS/TRACKING FOR REPAIR. THIS IS A CATEGORY B REPAIR. THIS IS A MAJOR REPAIR REPLACEMENT OF SEGMENT DONE ON NR 27 WO 92512
[MAIN DECK STUB FRAME IS CRACKED AT UPPER FLANGE AT 580 LBL 45.50 MAIN DECK STUB FRAME CRACKED AT UPPER FLANGE STA 580 LBL 45.50, 2026-07-01] ORG WRI 979 25-50 0563 MAIN CARGO DECK LEFT O/B SEAT TRACK DAMAGED AT STATION 579. LOCK ID B579. REPLACED SEGMENT USING E.A.#:F-5310-T0387768 PART: 1 (P1) TITLE: FUSELAGE - MAINFRAME - SEAT TRACK SPLICE REPAIR FROM STA 530 TO STA 610 AT LBL 45 ALONG WITH 757 SRM 53-00-52- 2R AND DRW 657N3399.
SEAT TRACK DAMAGE TO LOBES ONLY AND WITH IN DEFERAL LIMITS WITH NO EQUIPMENT INSTALLED WITHIN 3 INCHES IAW SRM 53-00-52-1A FIG 101 DETAIL XI SHEET 6.
THE L1 DOOR WILL NOT OPEN COMPLETELY. R & R THE L1 DOOR ROTARY SNUBBER UP TO BUT NOT INCLUDING STEP 3.G.(12) IAW AMM 52-11-10-4. COMPLETED INSTALLATION OF L1 DOOR, PNEUMATIC LINE. RECONNECTED AND SAFETY PIN REMOVED. INSTALLATION OF L1 ROTARY SNUBBER PER AMM 52-11-10-4. L1 DOOR OPS NORMAL.
L1 DOOR WILL ONLY OPEN HALF WAY. AMM: 52-11-08-4 PUT A/C BACK IN NORMAL CONFIG. OPENED AND CLOSED L1 DOOR MULTIPLE TIMES IAW AMM 52-11-00-2 AND FOUND HOLD OPEN LOCK LEVER CONTACTING TRIGGER CATCH BOLT. FOUND TRIGGER CATCH BOLT INSTALLED INCORRECTLY IAW AMM 52-11-08-4 SUB TASK 52-11-08-434-099. REMOVED AND REINSTALLED BOLT CORRECTLY IAW AMM 52-11-08-4. OPENED AND CLOSED L1 DOOR MULTIPLE TIMES WITH NO DISCREPANCIES NOTED.
ENGINE #1 I/B NACELLE STRUT INTERNAL STRUCTURE AT APROX PPSTA 140.0 HAS CORROSION ON SIDE SKIN DISCRIPANCY WAS ACCOMPLISHED ON NR N00271.
ENG #1 I/B NACELLE STRUT INTERNAL STRUCTURE THRU ACCESS PANEL # 433AL HAS CORROSION ON THE SKIN COMPLIED WITH EA # F-5450-T0384076 P1 TITLE: NACELLES/PYLON N0 1 PYLON, INBD PANEL, PP STA 163, INNER SKIN ASSY, CORROSION REPAIR
MAIN CABIN FLOOR BEAM AT BS 1681.0 RBL 24.75 WITH EVIDENCE CORROSION COMPLIED WITH EA # F-5310-T0384192 TITLE: FUSELAGE - MAINFRAME - REPAIR OF STA 1681 FLOOR BEAM LOWER CHORD CORROSION AT RBL 26
L.E. SLAT NO 1 INB MAIN TRACK AREA, INTERNAL SKIN WITH CRACK. FABRICATED, LOCATED AND DRILLED REPAIR PARTS SLAT #1 INB MAIN TRACK AREA, REMOVED SLAT #1 IAW B 757 AMM 27-81-02-4, INSTALLED REPAIR PARTS IAW B 757 SRM 57-43-01-2R FIG 201 REP 4, RE-INSTALLED #1 LE SLAT IAW B 757 AMM 27-81-02-4, TORQUE USED ID # 02007 DUE 10/02/25 (EA # F-5750-T0384212 P1 - RSC TRACKING ONLY)
STAB COMP BETWEEN STA 1787 TO 1825 STR 3R APU AIR INLET DOOR SURROUND ANGLE CORRODED.
RIGHT WING INB FLAP T/E BTW MF STA 223.86 TO MF 243.0 SUSPECT DELAMINATION. PERFORMED TAP TEST ON RT WING I/B FLAP T/E "MAIN FLAP DELAMINATION FOUND DIM = 3" LONG ,12"WIDTH OUT OF LIMIT IAW B757 SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 5 NOTE "L" IAW B757 SRM 51-10-06-2R, APPLIED PERMANENT REPAIR ON RH WING I/B FLAP T/E "MAIN FLAP " IAW B757 51-70-10-2R, REP 4 FIG 201, SHEET 1. THIS IS MAJOR REPAIR.
L1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L1 DOOR GUST LOCK SPLIT COLLAR, OPS CHECK GOOD, OK FOR SERVICE.
L1 DOOR HANDLE DIFFICULT TO OPEN/CLOSE. FOUND THAT THE UPPER AFT LATCH FITTING WAS WORN AND THE UPPER FORWARD ROLLER WAS DAMAGED. REMOVED AND REPLACED THE LATCH FITTING AND ROLLER THE LOWER DOOR GUIDE ARM SEEMS TO BE CAUSING THE DOOR TO NOT CLOSE CORRECTLY. REMOVED GUIDE ARM. COMPLETED INSTALL AND ADJUSTMENT OF L1 DOOR GUIDE ARM. GAPS AROUND DOOR CHECK GOOD. ADJUSTMENT ON THE UPPER AFT LATCH FITTING IN REFERENCE TO B757 AMM 52-11-00-5. DOOR OPERATES NORMALY.
WHILE PERFORMING SERVICE CHECK INSPECTION FOUND RH EMERGENCY LIGHTS WILL NOT ILLUMINATE. AMM: 33-51-07-2 USED TABLE TO CALCULATE THE TIME NECESSARY TO CHARGE THE BATTERY PER AMM WITH NO HELP. R&R RH EMERGENCY BATTERY PACK SUPPLY PER B757 AMM 33-51-07-2. OPS CHECK GOOD.
WHILE PERFORMING SERVICE CHECK INSPECTION FOUND RH EMERGENCY LIGHTS WILL NOT ILLUMINATE. R&R RH EMERGENCY BATTERY PACK SUPPLY PER B757 AMM 33-51-07-2. OPS CHECK GOOD.
CONFIRMED RT ENGINE FUEL LEAK. LOST APPROX 1800 POUNDS IN 30 MINS. SHUTDOWN RT ENGINE IN FLT. RT SIDE FUEL INDICATOR CONTINUED TO DECREASE EVEN WITH ENG SHUT DOWN. 3000 LBS SPLIT BETWEEN ENGINES BY THE TIME WE BLOCKED IN. NO REFERENCE REQUIRED CREW CONFIRMED THAT AN EMERGENCY WAS DECLARED, & THE RT ENG WAS SHUTDOWN IN FLT. USED FUEL STICKS FOR RT TANK TO VERIFY FUEL QTY REF MM 28-44-00-2 , TANK OVERHEAD IND IS CORRECT. NO NOTICEABLE FUEL ODOR AROUND ENG OR LEAKS ON GROUND. REMOVED AND REPLACED RT TANK FUELING SHUTOFF VALVE ACTUATOR. OPS/LEAK CHECKS GOOD AT THIS TIME. IAW AMM 28-21-12-4.
FWD CARGO COMPARTMENT FIRE EXTINGUISHER ARMED SWITCH FOUND DAMAGED AND BURNED FROM ELECTRICAL ARCING, CAUSING FAN CONTROL FWD CARGO AND LEFT RECIRC FAN CONTROL CIRCUIT BREAKERS TO TRIP. REMOVED AND REPLACED THE APU/CARGO FIRE CONTROL PANEL M10444
FWD CARGO COMPARTMENT FIRE EXTINGUISHER ARMED SWITCH FOUND DAMAGED AND BURNED FROM ELECTRICAL ARCING, CAUSING FAN CONTROL FWD CARGO AND LEFT RECIRC FAN CONTROL CIRCUIT BREAKERS TO TRIP. ENT BY: 202601 RPT BY:202601 REMOVED AND REPLACED THE APU/CARGO FIRE CONTROL PANEL M10444
L1 DOOR WAS VERY DIFFICULT TO OPEN. AFTER OPENING AND INSPECTING DOOR FRAME AREA, FOUND GOUGING AND METAL SHAVINGS ON ROLLER TRACK NEAR S10094 NO. 1 DOOR LOCK SENSOR. PERFORMED APPROVED REPAIR TO ROLLER TRACK NEAR S100094 NO. DOOR LOCK IAW AMM 52-11-37-8-99. GOUGE WAS IN LIMITS (0.040). CLEAN AREA AND PERFORMED HFEC INSPECTION TO REWORK ROLLER IAW NDT PART 6, 51-00-01/51-00-19. NO CRACKS NOTED. DOOR OPENS AND CLOSES NORMAL IAW AMM 51-11-00-2.
TE FLAP DISAGREE EICAS MESSAGE ON FINAL WHEN SELECTION FLAPS 25. PERFORMED GO AROUND, RAN QRH PROCEDURE. DECLARED AN EMERGENCY AND LANDED WITHOUT EVENT. ***EMERGENCY DECLARED*** FACT 19MAR24 02:46 SYR FIM: 27-51 FT 808 FIM: 27-51 FT 805 PERFORMED FSEU 1, 2 AND 3 BITE PROCEDURES. NO FAULTS ON ANY OF THE 3 BOXES. TROUBLE SHOT PER FIM 27-51 FT 808. FLAP OPERATION CHECKS NORMAL. OK FOR SERVICE.
WHILE WORKING WRI 25-60/8873 R-1 DOOR SLIDE LIGHT INOP. INSTALLED AND ADJUSTED PROXIMITY ACTUATOR ON R-1 DOOR FWD GIRT BAR SLIDER IAW AMM 25-66-11-2. REMOVED CYCLINDER SAFETY PIN AND PLACED IN STORAGE POUCH ON ESCAPE SLIDE AND REINSTALLED SLIDE COVER IAW AMM 25-66-01-4. SLIDE LIGHT AND GIRT BAR/DOOR OPS CHECK NORMAL IAW AMM 25-66-11-2.
R1 DOOR FORWARD GIRT BAR LOCK FOUND MISSING ON ARRIVAL IN GSO. REPLACED FWD GIRT BAR LOCK ASSY. DOOR WILL NOT DISARM FULLY AFT BAR LOCK WILL NOT DISENGAGE FULLY. R1 DOOR CONFIGURED FOR MEL. ACCOMPLISHED R1 DOOR GIRT BAR ADJUSTMENT IAW MM GIRT BAR OPERATES NORMALLY, FULLY ENGAGING AND DISENGAGE.
PDIS 979 27-50 8817 07SEP23 MSY FACT U ON APPROACH, WHEN SELECTING FLAPS 25, GOT TE FLAP DISAGREE EICAS, AND FLAPS APPEARED STUCK JUST PRIOR TO 25 INDICATION. WENT AROUND, RAN QRH AND LANDED WITHOUT ISSUE. ***EMERGENCY DECLARED*** FIM: 27-51 FT 808 PERFORMED BITE CHECK WITH NO FAULT. NOTHING TRIPPED ON #4 FLAPS TRANSMISSION OVERLOAD INDICATOR. GVI OF TRANSMISSION AND JACKSCREW WAS ACCOMPLISHED. FLIUD WAS FULL. CYCLED FLAPS MULTIPLE TIMES WITH NO DEFECTS NOTED. A/C OK FOR SERVICE.
TAIL COMPARTMENT, APU INLET DUCT IS DELAMINATED ON INTERNAL SURFACE BETWEEN BS1825 AND BS1865. REPAIRED APU INLET DUCT BY PERFORMING WET LAY UP REPAIR PER B757 SRM 51-70-17-0G AND FEDEX EA # F- 4900-T0375670
NOSE WHEEL WELL PANEL 117AL HAS MINOR SURFACE CORROSION. BLENDED CORROSION FROM PANEL, ORG MATERIAL WAS .100, REMOVED .009 OF MATERIAL, .091 REMAINS, FOUND TO BE IN LIMITS PER B757 SRM 53-10-14-1A DETAIL IV. ALODINED PANEL PER B757 AMM 51-21-04. PRIMED PANEL PER B757 AMM 51-21-14, PAINTED PANEL PER B757 AMM 51-21-15.
#2 ENGINE INLET COWLING HAS CORROSION IN NUMEROUS SPOTS (PART RACK) OUT OF LIMITS IAW BOMBARDIER CMM 71-11-50-300-806-A01, RECIVED NEW PART/PART RACK ITEM PO#1067549.1, RB211-535E4 ENGINE ROLLS ROYCE PART NUMBER
MAIN CABIN CARGO FLOOR SEAT TRACK @ LBL24.75, APPROX STA 657 HAS MULTIPLE GOUGES AS MARKED REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A, REPAIRED SEAT TRACK IAW B757 SRM 53-00-52-2R - REPAIR #3 - OPTION#2
DURING SEAL REPLACEMENT ON N/R 32113, FEDEX NR N00326 FOUND CORROSION ON SKIN UNDER ELEPHANT EAR FAIRING ON R.WING I/B MAIN FLAP. REMOVED SKIN PLATE, FABRICATED NEW SKIN PLATE PER BAC DWG 113N2402 REV A,. REINSTALLED SKIN PLATE PER BAC DWG 113N2402. AND FEDEX EA # F-5750-T0375725 TITLE : WINGS - FLIGHT SURFACES - RH INBD MAIN FLAP, LOWER SKIN, MF STA 74 - 77, FABRICATION, ALTERNATE SURFACE PREPARATION.
RIGHT HORIZONTAL ACCESS PANEL 345BB IS CRACKED ACCOMPLISHED PERMANENT REPAIR OF RIGHT HORIZONTAL ACCESS PANEL 345BB IAW B757 SRM 55-20-01-1A, 55-20-01-2R AND 51-70-05-0G
THE SLIDE LIGHT ON THE L1 ENTRY DOOR IS BURNED OUT. DOES NOT ILLUMINATE WHEN DOOR ARMED AND BULB TESTS BAD DURING INSPECTION OF L1 DOOR GIRT BAR, FOUND LEAF SPRING ON GIRT BAR DAMAGED AND OBSTRUCTING FWD GIRT BAR SLIDER. REMOVED AND REPLACED GIRT BAR ASSY. ALL OPS CHECKS GOOD AT THIS TIME. SLIDE LIGHT ILLUMINATES PROPERLY. ADJUSTMENT AND TESTS CHECKS GOOD AT THIS TIME
RECEIVED A TRAILING EDGE FLAPS DISAGREE WHEN LOWERING THE FLAPS TO FLAPS 25. THE FLAPS APPEARED TO BE AT 24. PERFORMED GO AROUND AND EXECUTED QRH TO AN UNEVENTFUL LANDING. ***EMERGENCY DECLARED*** INSPECTED AND LUBED LEFT AND RIGHT FLAP TRACKS AND CARRIAGES IN REF TO AMM. INSPECTED AND CLEANED FLAP RESOLVERS. NO DEFECT NOTED. PERFORMED OPERATION CHECK OF THE FLAP SYSTEM MULTIPLE TIMES. OPS CHECK NORMAL.
ESCAPE SLIGHT ENGAGEMENT LIGHT FOR L1 DOOR INDICATION IS UNRELIABLE AND INOP PART 18MAR22 14:35 OKC U IDENTIFIED PARTS SENSOR MPN: 60B40018-41. L1 (IDENTIFY L1 AND/OR R1) ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VERIFY AND RECORD IN AML/EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE." GIRT BAR ENGAGES NORMALLY. FOUND DEBRIS AROUND FORWARD SENSOR S10215 AND REMOVED. SUSPECT SENSOR IS FAULTY. ORDERED SENSOR C/7309400. REMOVED AND REPLACED FORWARD GIRT BAR PROXIMITY SWITCH IAW B757 AMM 25-66-11-2. OPS CHECKS NORMAL. PART REMOVED - GIRT BAR PROXIMITY SWITCH, P/N 8102-0401.
RI DOOR SLIDE RAFT GIRT BAR HANGING DOWN BAR FWD LOCKING BLOCK SECURE CLIP DAMAGE. REMOVED & REPLACED THE R1 DOOR EVACUATION SLIDE "GIRT BAR" PER B757 AMM 25-66-10-2. CHECKS OK.
ON APPROACH, "TE FLAP DISAGREE" LIGHT AND EICAS MSG WHEN GOING FROM FLAPS 15 TO 20. RAN QRH AND LANDED FLAPS 20. REF FIM 27-51 FT 808, NR 1 FSEU HAS INTERMITTENT FAIL DURING BITE CHECK. NO OVERLOAD INDICATORS TRIPPED. REMOVED AND REPLACED NR 1 FSEU AND CHECK NORMAL REF MM 27-51-01-2. OK FOR SERVICE.
L1 SLIDE LIGHT WILL NOT ILLUMINATE FOUND L1 DOOR SLIDE LANYARD HANGING DOWN- STOWED LANYARD-DOOR SLIDE ARMS AND DISARMS NML- REF: B757 M/M 25-66-10-2
UPON CLOSING THE MAIN ENTRY DOOR COULDNT GET THE SECURE LIGHT ON (SLIDE LIGHT ON). FOUND SLIDE STATIC LINE LOOSE -RESTOWED SAME- L1 DOOR GIRT BAR AND LIGHT CHECKS GOOD- REINSTALLED DOOR SLIDE COVER- DOOR SLIDE AND DOOR ASSIST BOTTLES SAFETIES RMVD- REF: B757 M/M 25-66-01-4
VELCRO EVAS STRIP ON CAPTAIN GLARE SHIELD IS SEPERATING. REPLACED VELCRO LOOP FASTENER. REF AMM 25_62_00_8_0 A/C OK FOR SERVICE.
EVAS VELCRO STRIP ON F/O GLARE SHIELD MISSING REPLACED VELCRO LOOP FASTENER. REF AMM 25_62_00_8_0 A/C OK FOR SERVICE.
PDIS 979 25-60 5797 12DEC19 MEM FACT U LOGPAGES:2325689 PART OF THE DOOR SEAL ON THE LEFT CREW ENTRY DOOR IS DANGLING FACT 12DEC19 10:28 MEM U RE-SECURED L1 DOOR SLIDE LANYARD REF AMM 25-66-01-4-0. NO DEFECTS NOTED. A/C OK FOR SERVICE.
FWD WET AREA PANEL 221MBF HAS DAMAGED FIBERS ON UPPER SURFACE FABRICATED NEW FWD WET AREA FLOOR PANEL 221MBF IAW FEDEX DWG # SRZ-25-005 REV R
FORWARD WET AREA CORROSION STA 345 FLOORBEAM UPPER SURFACE OF UPPER CHORD, FORWARD AND AFT FLANGES, APPROX LBL 5 - LBL 23 AND LBL 56. BLENDED OUT CORROSION AREA AT FLOORBEAM STA 345 UPPER SURFACE OF UPPER CHORD AND FOUND OUT OF LIMITS AT LBL 5 AND LBL 23 IAW SRM 53-00-51-1A FIG 101 DET IV, CUT AND REMOVED FLOORBEAM UPPER CORD, LOCATED, DRILLED AND TRIMMED T CHORD AND FABRICATED REPAIR SPLICES (ANGLES AND STRAPS) AND INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51-2R REPAIR 10.
ON APPROACH TO JFK WHEN FLAPS 25 SELECTED, "TE FLAP DISAGREE" EICAS MESSAGE. EXECUTED GO-AROUND, COMPLIED WITH QRH LANDED UNEVENTFUL @ JFK. EMERGENCY DECLARED. T/S PER FIM 27-51 FAULT TREE 805 AND 27-51 FAULT TREE 808. FOUND SLIGHT DEBRIS ON FLAP HANDLE DETENTS. REF FIM 27-51 FAULT TREE 808 "TE FLAPS DISAGREE" OPERATED EACH DETENT OF FLAPS NUMEROUS TIMES WITH NO FAULTS. OPERATED FLAPS WITH ENGINES RUNNING PER JRH - ENGINE DRIVEN HYDRAULIC PUMPS AND ELECTRIC HYDRAULIC PUMPS OPERATIONAL. NO FAULTS NOTED. FLAPS AND HYDRAULICS INDICATION AND OPERATION NORMAL. PERFORMED VISUAL INSPECTION OF FLAP GEARBOXES AND FLAP DRIVES. NO OBSTRUCTION OR DAMAGE NOTED. INTERROGATED FSEU-1, FSEU-2 AND FSEU-3 AND FOUND NO EXISTING FAULTS OR LAST LEG FAULTS. NO 30-DAY HISTORY. A/C OK FOR CON'T SVC.
BURNING ODOR FOLLOWED BY EQPT OVERHEAT EICAS AND EQUIPMENT COOLING OVERHEAT LIGHT. RAN QRH, OVHT INDICATION REMAINED ON. LANDED AIRCRAFT, NO OTHER PROBLEMS. REMOVED AND REPLACED THE NR 1 FWD EQUIPMENT COOLING SUPPLY AIR FAN IAW MM 21-58-06-4, OPS CHECKED GOOD NO FAULTS NOTED AT THIS TIME.
BULK CARGO DOOR EXTERIOR SKIN HAS GOUGE ABOVE DOOR HANDLE CUTOUT. REPAIRED BULK CARGO DOOR EXTERIOR SKIN ABOVE DOOR HANDLE CUT OUT AS REQUIRED IAW EA F-5230-T0336231 P1.
L1 DOOR SLIDE ARMED LIGHT IS ILLUMINATED WITH THE HANDLE IN THE DISARMED POSITION. R & R THE SENSOR S10215 IAW SWPM 20. PERFORMED ADJUSTMENT AND TEST IAW MM 52-11-25-5. OPS CHECKED GOOD.
AT 10,000, CLIMBING IN CLIMB, POWER LEFT ENGINE FUEL FLOW GOT HIGH AND EGT YELLOW. RAN QRH AND RETURNED TO AIRPORT. ONLY REASON ENGINE DID NOT GO INTO RED EGT IS PILOT ACTION. REMOVED AND REPLACED THE NR 1 ENG P1 PROBE IAW AMM 73-21-04-4, OPS NORMAL IAW 30-34-00-5.
LEFT ENGINE, HIGH EGT AND FUEL FLOW AT 10,000 FT WHEN CHANGING POWER FROM CLIMB 2 TO NORMAL CLIMB. RAN THE QRH, CONTINUED TO OPERATE ENGINE (LEFT) AT LOWER POWER AND RETURNED TO AIRPORT. INSPECTED NR 1 ENGINE INLET AND EXHAUST WITH NO DEFECTS NOTED IAW MM 72-00-00-6, INSPECTED THE NR 1 ENGINE MASTER CHIP DETECTOR IAW MM 79-21-03-04, NO DEFECTS NOTED. EGT EXCEEDANCE OF 810 FOR .8 SECONDS IAW EICAS WITHIN LIMITS IAW FIM 71-05-00-1, FAULT TREE 824 FIG 121. AIRCRAFT OK FOR CONTINUED SERVICE.
GEAR DOORS EICAS WITH DOOR ANNUCIATOR, AFTER TAKEOFF. WITH GEAR HANDLE PLACED IN THE OFF POSITION. INSPECTED LEFT AND RIGHT MAIN GEAR DOORS, STOPS, STOP PLATES, AND SENSORS. FOUND LEFT AND RIGHT FORWARD STOP BOLTS WORN BEYOND LIMITS. LEFT READS .017, RIGHT READS .030. MINIMUM LIMIT IS .035. FOUND STOP PLATES WORN, UNABLE TO MEASURE WITH PLATE INSTALLED ON ACFT, BUT NOTICABLY WORN. LEFT SIDE DOOR SHOWS AREA WHERE PROX SENSORS WERE IMPACTING DOOR. ALL OTHER INSPECTION ITEMS CHECK NORMAL IAW AMM 32-12-00-6 ALL STEPS COMPLETED WITH NO DEFECTS NOTED EXCEPT NOSE GEAR CLOSE PROXIMITY SENSORS OUT OF ADJUSTMETN IAW 32-61-03. NO FUTHER ACTION REQUIRED.
WHILE SECURING AIRCRAFT FOUND L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. DOOR WOULD NOT LOCK IN THE OPEN POSITION. REMOVED AND REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR IAW AMM 52-11-08-8. DOOR OPS CHECKED GOOD
L1 DOOR SLIDE ARM LITE INOP. CLEANED AND REMOVED DEBRIS AWAY FROM THE FWD AND AFT L1 DOOR GIRT BAR PROX SENSORS. SLIDE LIGHT OPERATES NORMALLY WHEN ARMED AND DISARMED PER AMM 25-66-11-2. NO HISTORY, OK TO CONTINUE.
ON APPROCH, PASSING 500 FEET AGL, RECEIVED TOO LOW GEAR CAWS. LANDING GEAR INDICATORS DISPLAYED GREEN THREE DOWN. PERFORMED GO AROUND, SECOND APPROACH ALL INDICATIONS NORMAL. ON POSTFLIGHT STATUS PAGE DISPLAYED -LDG GEAR MONITOR -GEAR DISAGREE -L EEC BITE. PERFORMED FIM 32-09-03. FAULT TREE 805. NO FAULT NOTED INSPECTED MLG AND NLG NO VISIBLE DAMAGES NOTED. GOOD FOR SERVICE.
LEFT SLIDE ANNUNCIATOR ARM LIGHT DOES NOT ILLUMINATE WHEN ARMED. CLEANED GIRT BAR PROXIMITY SWITCHES, TESTS NORMAL IAW AMM 25-66-11-2.
L1 ENTRY DOOR, SLIDE LIGHT WILL NOT ILLUMINATE WHEN ARMED. FOUND ARMING LINK AT L1 LOWER DOOR CAM ASSEMBLY, BOLT LOOSE CAUSING SLOP IN THE MECHANISM. TIGHTENED NUT ON BOLT & PERFORMED OPERATIONS TEST OF GIRT BAR MECHANISM.
L1 DOOR SLIDE LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-66-05-A CATEGORY C, EXPIRATION 13 NOV 15. ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE. FOUND THE GIRT BAR CRANK ADJUSTMENT NUT & CAM TO BE LOOSE, ON THE AFT SIDE OF THE DOOR. TIGHTENED & RIGGED IAW AMM 52-11-25-5. OPERATIONS CHECKED SATISFACTORY. OK FOR SERVICE.
AFTER TAKEOFF GEAR HANDLE DID NOT MOVE PAST THE OFF POSITION WHEN RETRACTING GEAR. GEAR DISAGREE EICAS LIGHT ILLUMINATED. QRH RED TABS DIRECTED, THE GEAR WILL NOT MOVE UP CHECKLIST TO BE ACCOMPLISHED. AFTER RETRACTING THE GEAR USING THE LOCK OVERRIDE SWITCH, OPERATION WAS NORMAL FOR THE REMAINDER OF FLIGHT. TROUBLE SHOT IAW FIM 32-30 FAULT TREE 820,THE BITE TEST OF THE PSEU REVEALED FAULT CODE 424 LG LEVER UP SYS 2. REPLACED RELAY K209 IAW AMM 32-09-02. NO FAULTS OR EICAS MSGS DISPLAYED AFTER SYS TEST.
TRAILING EDGE FLAP DISAGREE. FLAPS STOPPED AT GREATER THAN 20 BUT LESS THAN 25. WHEN POWER SWITCHED TO APU FLAPS CYCLED BACK TO 20 & DISAGREE WENT AWAY. PERFORMED BITE OF ALL 3 FSEU'S IAW FIM 27-51, NO EXISTING FAULTS. FLIGHT DECK TESTED GOOD. PERFORMED TE FLAP SYS ADJUSTMENT TEST IAW AMM 27-51-00-5, NO DEFECT NOTED. SUSPECT FLAP HANDLE NOT IN DETENT IAW FIM 27-51 FIG 808. ACFT OK FOR SERVICE.
SLIDE LIGHT ABOVE LT ENTRY DOOR HAS A LAMP OUT. RELAMPED IAW WITH SMP 33.
TO GET SLIDE LIGHT ON DURING CLOSE-UP FIRST OFFICER HAD TO OPEN & RECYCLE DOOR L1 TO GET A GOOD SLIDE ARMED INDICATION. LUBED L1 DOOR GIRT BAR MECHANISM IAW AMM 12-21-18-3, ARMING SLIDE TESTED GOOD.
EMERGENCY LIGHT ABOVE L1 DOOR DIM & GOES OUT. R & R BATTERY PACK FOR LT SIDE EMER LIGHT IAW AMM 33-51-07-2. OPERATIONS CHECKED NORMAL.
UPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND HONEYCOMB HAS BEEN DISTORTED ON THE OTBD END AT STABILIZER STA 224. SKIN REPAIRED IAW EAF-5510-T0303533. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DENT IN RT HORIZONTAL STABILIZER UPPER SURFACE BETWEEN FRONT SPAR AND REAR SPAR, STAB STA 200 -224. DENT REPAIRED IAW EAF-5510-T0303533. . REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
EMPENNAGE RT SIDE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER STA 128 -176. THE UPPER SKIN BETWEEN FORWARD SPAR AND FWD AUX SPAR ON THE LOWER SKIN BETWEEN STABILIZER STA 128-176. REPAIR OUT IAW EAF-5510-T0303533 STABILIZERS-757 HORIZONTAL STABILIZER-MAIN TORQUE BOX UPPER SKIN PANEL REPAIR. REFER TO N02009 FOR WORK DETAILS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RT SIDE OF EMPENNAGE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND NUT PLATE HAS ELONGATED HOLE AT INBD LOGO LIGHT. REPAIRED IAW EA F-5510-T0303569. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RT SIDE HONEYCOMB INTERIOR SIDE, LOWER SIDE OF UPPER SKIN, DELAMINATED. REMOVED AND REPAIRED OUT IAW EA F-5510-T0303533. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RT SIDE EMPENNAGE, AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER BS 176-224. REPAIRED IAW EA F-5510-T0303533. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.
NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT BS 620-640. DAMAGE REMOVED ANDFOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II, REV 109 AND REPAIRED IAW EA F-5330-T0302663. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540-520, 540 -560, STR 26L-26R EXTERIOR SKIN NICKS AND SCRATCHES. REMOVED, FOUND OUT OF LIMIT AT STA 523, ABOVE STR 28L AND STA 529 BELOW STR 27L IAW SRM 53-00-01, FIG 101 DETAIL II, REV 109 AND REPAIR CARRIED OUT IAW EA F-5330-T0302746, FUSELAGE - PLATES & SKINS - FUSELAGE SKIN PANEL REPAIR , STA 510-STA 550, S27L-S28L. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
SKIN DENTED AT BS 460-480, STR 27L- 28L, PUNCTURED THROUGH. REPAIRED IAW EA F-5240-T0303070. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
BS 1640 BL 0 - LBL 30, FLOORBEAM UPPER FLANGE FOUND CHAFED AROUND FASTENER HOLES. FLOORBEAM REMOVED IAW SRM 51-40-02 REVISION 109. NEW FABRICATED FLOORBEAM INSTALLED IAW DWG 146N5089 SHEET 1 REV B. REPAIR IS CLASSIFED MAJOR IAW GMM 6-2-100.
BS 1640, BL 0 TO RBL 45.5, FLOORBEAM UPPER FLANGE FOUND CHAFED. FLOORBEAM REMOVED IAW SRM 51-40-02 REVISION 109 AND NEW FABRICATED FLOORBEAM INSTALLED IAW DWG 146N5089 SHEET 1 REVISION B. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.
FWD E & E BAY BS 255, RBL 3, FRAME WEB CHAFED. REPAIRED IAW EA F-5310-T0303276 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
BS 1661, BL 0 - RBL 51.5, FLOORBEAM UPPER FLANGE LOWER SURFACE FOUND CORRODED AROUND FASTENER HOLES. CORRODED FLOORBEAM REMOVED AND REPLACED WITH NEW FABRICATED IAW DWG 146N5110 SHT.2 REV.B AND INSTALLED IAW DWG 146N5090 SHT.5 REV.- AND DWG 146N5500 SHT.1 REV.G. REPAIR IS MAJOR.
CENTER WING TANK UPPER PANEL FOUND CORRODED BS 1016, RBL 63. REPAIRED IAW EA F-5730-T0302786 PART 1 .
RT CREASE BEAM INBD ANGLE BS 1320 -1340 FOUND CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED IAW DWG 146N8322 SHT.1 REV.F. REPAIR IS MAJOR.
FLOORBEAM UPPER TEE FOUND CORRODED AT UPPER SURFACE BS 365.25, RBL 24.75 - 45.5. REMOVED AND REPLACED IAW SRM 51-40-02 REV 109 AND DWG 141N5112 SHT 1 REV D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STA 365.25 BL0 -RBL 24.75 FLOORBEAM UPPER CHORD, UPPER SURFACE FOUND CORROSION AT EDGE. REMOVED AND REPLACED IAW SRM 51-40-02 REV 109 AND DWG 141N5112 SHT 1 REV D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FLOORBEAM UPPER TEE FOUND CORRODED AT UPPER AND LOWER SURFACES BS 377.7, BL 0-LBL 20. REMOVED AND REPLACED FLOORBEAM FABRICATED IAW DWG 141N5123 SHT 1 REV A AND INSTALLED IAW DWG 141N5113 SHT 1 REV F AND SRM 51-40-02 REV 109. REPAIR IS MAJOR.
FLOORBEAM UPPER TEE BS 377.7, LBL 58 FOUND CORRODED AT UPPER SURFACE. REMOVED AND REPLACED FLOORBEAM FABRICATED AS PER DWG 141N5123 SHT.1 REV.A AND INSTALLED IAW DWG 141N5113 SHT.1 REV.F AND SRM 51-40-02 REV.109. REPAIR IS MAJOR.
SEAT TRACK BS 1600 -1640 RBL 45.5 FOUND CHAFED AT THE CROWN AND BOTTOM. REPAIRED IAW SRM 53-00-52 REPAIR 1 FIG. 201 REV 109. REPAIR IS MAJOR.
L2 DOOR LOWER SILL INBD ANGLE BS 690 -730 FOUND CORRODED AND CHAFED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.
R2 DOOR LOWER SILL INBD ANGLE BS 720 -730. FOUND CHAFED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.
L2 DOOR LOWER SILL INBD CHORD BS 730-755 FOUND CORRODED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.
MAIN E/E BAY ACCESS DOOR INNER SKIN CRACKED AT THE HOLE EDGE. REPAIRED IAW EA F-5240-T0303070. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
BS 1681, RBL 39, DECK PLATE ONE FASTENER HOLE ELONGATED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR IS MAJOR
BS 1681-1720, RBL 39, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D.
BS 1681, BL 0 -LBL 50, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.
BS 1715, LBL 17 - RBL 17, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 & REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.
BS 324, LBL 20, FLOORBEAM STIFFENER FOUND GOUGED AT EDGE. REPAIRED IAW EA F-5320-T0302984 PART 1. REPAIR IS MAJOR.
CABIN - STA 365.25-377.7 LBL 24.75 FLOORBEAM STABILIZER STRAP FOUND CRACKED. REPAIRED IAW EO F-5320-T0302912A PART 1.
BS 500 FRAME OTBD FAILSAFE FOUND CORRODED AT EDGE S17R. REPAIRED IAW EA F-5310-T0302910 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
CABIN, BS 620, STRINGER 17R FRAME OTBD FAILSAFE FOUND CORRODED AT EDGE. FAILSAFE REMOVED AND REPLACED IAW DWG 146N8513 SHT.1 REV.A AND INSTALLED IAW DWG 143N8512 SHT.1 REV.J. REPAIR IS MAJOR.
BS 755 -780 LT CREASE BEAM INBD ANGLE FOUND CHAFED AT UPPER SURFACE. REPAIRED IAW EA F-5310-T0302749, PART 1. REPAIR CLASSIFIED MINOR PER BMM 6-2-100.
NR 1 PYLON STRUT MID BULKHEAD LOWER FLANGE OTBD FWD SIDE AT PYLON STA 174.3. FOUND SHIM FRAYED AND MIGRATED. NDT INSPECTED-MID BULKHEAD FOUND CRACKED AT ATTACHMENT TO LOWER ANGLE. DAMAGED SHIM REMOVED AND SOLID TAPERED SHIM FABRICATED AND INSTALLED PER SRM 54-50-90 FIG 201 REPAIR 7 REV 109. CRACK REPAIRED PER EA F-5450-T0302438. REPAIR IS MAJOR.
FUSELAGE SKIN HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540 -560. DAMAGE REMOVED & FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 109 AND REPAIRED IAW EA F-5330-T0302746. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
FUSELAGE EXTERIOR SKIN LT SIDE SCRATCHED ALONG THE PERIMETER OF THE WING TO BODY FAIRING MATING SURFACE AT BS 780-760, STRINGER 25-27L. REMOVED SCRATCHES AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIGURE 101 DETAIL 2 REV. 109 AND REPAIRED IAW EA F-5330-T0302661. REPAIR CLASSIFIED MINOR.
SKIN HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 600 -620. DAMAGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 109 AND REPAIRED IAW EA F-5330-T0302663. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
BS 333.45, LBL 45.5 - 64, FLOORBEAM UPPER TEE FOUND CORRODED AT UPPER AND LOWER SURFACES. REMOVED AND REPLACED WITH NEW BEAM FABRICATED IAW DWG 141N5120 SHT.1 REV.A AND INSTALLED IAW EWG 141N5110 SHT.1 REV.B. REPAIR IS MAJOR.
BS 310-324, R1 DOOR LOWER SILL INBD ANGLE FOUND CORRODED AT UPPER SURFACE. CORROSION REMOVED AS PER SRM 51-10-02 REV 109 FOUND EXCEED LIMIT AS PER SRM 53-10-158 ALLOWABLE DAMAGE 1 FIG 101 REV 109. I/B ANGLE REMOVED AND REPLACED AS PER SRM 51-40-02 REV 109 AND DWG 141N8422 SHT 1 REV R. REPAIR CLASSIFIED AS MAJOR.
BS 740 -752, R2 DOOR LOWER SILL WEB FOUND CORRODED AT LOWER SURFACE, AROUND FASTENER HOLES. CORROSION REMOVED AS PER SRM 51-10-02 REV 109. MATERIAL REMOVED 0.012" FOUND EXCEED LIMIT AS PER SRM 53-30-15 ALLOWABLE DAMAGE 1 FIG. 101 REV. 109. DOOR LOWER SILL WEB REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 109 AND DWG 143N8322 SH 1 REV. K WITH FABRICATED WEB. NEW DOOR LOWER SEAL WEB FABRICATED AS PER DWG 143N8322 SH 1 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FUSELAGE SKIN DENTED BS 760-780, S15-16L. REPAIRED IAW SRM 53- 00-01 FIG 201 REPAIR 16 REV 109. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
BS 755-780 RT CREASE BEAM INBD ANGLE FOUND CORROSION AT UPPER & LOWER SURFACES AROUND FASTENER HOLES. REPAIRED IAW EA F-5310-T0302508. REPAIR CALSSIFED MAJOR PER GMM 6-2-100.
BS 664-690, L2 DOOR LOWER SILL INBD ANGLE FOUND CORRODED AND CHAFED AT UPPER SURFACE. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT 1 REV K. MAJOR REPAIR.
BS 1100, S8-9L, FRAME INNER FLANGE CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 109. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 REV 109. REPAIRED IAW SRM 53-00-07 REPAIR 3 FIG 201 REV 109. REPAIR CLASSIFIED AS MAJOR.
BS 680 -684 R2 DOOR LOWER SILL INBD ANGLE FOUND CHAFED AND CORRODED AT UPPER SURFACE AND CORNER. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 109 AND DWG 143N8322 SHT 1 REV K. MAJOR REPAIR.
BS 1340 -1360, RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND FIVE FASTENER HOLES. REMOVED AND REPLACED WITH NEW ANGLE IAW DWG 146N8322 SHT.1 REV F. MAJOR REPAIR.
BS 1320-1360, LT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED WITH NEW ANGLE IAW DWG 146N8322 SHT.1 REV.F. MAJOR REPAIR.
BS 1715, LBL 29 - 50, DECK PLATE UPPER SURFACE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 109. FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG. 101 REV. 109. DECK PLATE REMOVED IAW SRM 51-40-02 REV. 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV. D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
BS 780 -830 LBL 45.5 SEAT TRACK FOUND CHAFED AT CROWN AND BOTTOM OF THE TRACK, GOUGE MARK AT CROWN BS 790, 800, & 814 - 824. REPAIRED IAW SRM 53-00-52, REPAIR 1, FIG.201, REV.109. MAJOR REPAIR.
BS 1000 - 1040, RBL 45.5 SEAT TRACK CROWN CHAFED. REMOVED IAW SRM 51-10-02 REV 109. FOUND EXCEEDED LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 109. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG 1201 REPAIR 4 REV 109 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
BS 440 RBL 45.5 SEAT TRACK FLANGE FOUND CORRODED AT UPPER SURFACE. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG 201 REAIR 1 REV 109. REPAIR IS MAJOR AS PER GMM 6-2-100.
BS 1621-1625, RBL 45.5 SEAT TRACK OTBD FLANGE HAS A CUTOUT. REPAIRED IAW SRM 53-00-52 REPAIR 1 FIG. 201 REV 109. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
BS 1320 -1350 LBL 24.75, SEAT TRACK FOUND CHAFED AT THE CROWN AND BOTTOM OF TRACK. REPAIRED IAW SRM 53-00-52 REPAIR 1 FIG. 201 REV. 109. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
BS 1320-1350, RBL 24.75, SEAT TRACK FOUND CHAFED AT THE CROWN AND BOTTOM. EXCEED LIMITS IAW SRM 53-00-52 FIG.101 REV. 109. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1 REV. 109. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
FUSELAGE HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 1480-1500. REPAIRED IAW SRM 53-00-01 FIG 201, REPAIR 16 REV.109. REPAIR IS CAT.B, MAJOR.
EMPENNAGE RT SIDE AFTER REMOVAL OF APU INLET HOUSING ASSY FOUND CORROSION ON THE FORWARD SIDE AT BS 1825 BETWEEN STRINGER 3 AND 6. CORROSION REMOVED & FOUND OUT OF LIMITS AS PER SRM 53-80-15 FEG 101 DETAIL II REV 109 AND REPAIRED IAW SRM 53-80-15 FIG 202 DETAIL 1 REPAIR 1 REV 109. MAJOR REPAIR.
BS 1280, S10-14L, FRAME FOUND GOUGED. FOUND EXCEED LIMITS IAW SRM 53-00-07 FIG 101. REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 3 REV.109. REPAIR CLASSIFIED AS MAJOR
BS 1280, S12 - 14R, FRAME FOUND GOUGED. FOUND EXCEED LIMITS IAW SRM 53-00-07 FIG 101 REV. 109. REPAIRED IAW SRM 53-00-07 REPAIR 3 FIG 201 REV. 109. REPAIR CLASSIFIED AS MAJOR.
RIGHT WING UPPER SKIN FOUND CORRODED AT OVERWING FILL PORT ADAPTER MATING SURFACE. REPAIRED IAW EA F-5730-T0302182 PART 1. REPAIR IS MAJOR.
BS 365.25-418, RBL 45.5 SEAT TRACK CROWN SUPPORT FOUND CORROSION AT UPPER SURFACE. SEAT TRACK REMOVED AND REPLACED IAW DWG 141N5130 SHT.2 REV.E. REPAIR IS MAJOR.
BS 377.7-418 LBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORRODED AND CHAFED AT UPPER SURFACE. SEAT TRACK REMOVED AND REPLACED IAW DWG 141N5131 SHT.4 REV.D AND INSTALLED IAW DWG 141N5130 SHT.4 REV.B. REPAIR IS MAJOR.
BS 377.7-418 LBL 45.5 SEAT TRACK CROWN FOUND CORRODED AT UPPER AND LOWER SURFACES. SEAT TRACK REMOVED AND REPLACEDIAW DWG 141N5131 SHT.4 REV.D AND INSTALLED IAW DWG 141N5130 SHT.4 REV.B. REPAIR IS MAJOR.
BS 365.25-418, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORRODED AT UPPER SURFACE. SEAT TRACK REMOVED AND REPLACED IAW DWG 141N5130 SHT.2 REV.E. REPAIR IS MAJOR.
LEFT L/E FRONT SPAR VERTICAL STIFFENER, FOUND CHAFED. REMOVED AND REPLACED IAW DWG 112N2038 SHT 1, REV -, AND DWG 112N2002 SHT 6, REV D.
BS 1640, RBL 45.5 - 51.5, FLOORBEAM UPPER FLANGE LOWER SURFACE FOUND CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED IAW DWG 146N5109 SHT 1, REV A AND INSTALLED IAW DWG 146N5089 SHT 1, REV B. REPAIR IS MAJOR.
BS 1660, LBL 20-25, FLOORBEAM UPPER FLANGE LOWER SURFACE, FOUND CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED IAW DWG 146N5110 SHT 2, REV B AND INSTALLED IAW DWG 146N5090 SHT 5, REV- AND DWG 146N5500 SHT 1, REV G. REPAIR IS MAJOR.
CORROSION ON SKIN STRAP AT BS 1790, BETWEEN STR 3-6R. APU INLET FWD SIDE SKIN STRAP CORROSION VISUALLY FOUND THAT EXCEEDED LIMIT IAW SRM 51-10-*02, REV 109, CORRODED STRAP. R & R WITH NEW STRAP. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
EMPENNAGE, RT SIDE-SUPPORT ANGLE HAS CORROSION AT BS 1790-1825 ON STR 6R. APU INLET FWD SIDE SUPPORT ANGLE CORROSION FOUND. THROUGH OUT OF LIMIT IAW SRM 51-10-02, REV 109 CORRODED SUPPORT ANGLE REMOVED IAW SRM 51-40-02, REV 109. SUPPORT ANGLE FABRICATED IAW DWG NR 148N3152, SHT 1, REV AND INSTALLED IAW DWG 148N3105, SHT 1, REV REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.