N974FD

Part: UNKNOWN — ODOR (COCKPIT) · airframe 74,411 hrs · 26,369 cycles

EXTREMELY STRONG ELECTRICALLY BURNING ODOR IN COCKPIT, DURING CLIMB AROUND 25,000 FT. ON ENTRY NO ODOR PRESENT.. CHECKED FOR CBS TRIPPED IN COCKPIT, ALL CLOSED. INSPECTED E & E BAY, OPENED ACCESS PANELS, FOUND NO EVIDENCE OF ODOR. FOUND LT LOGO LIGHT CB TRIPPED, RESET IAW MM 20-60-01-2. INSPECTED ENGINES FOR LEAKS, NONE NOTED. OPENED LT & RT A/C BAYS, INSPECTED PACKS, DUCTING & SURROUNDING AREA, NO DEFECTS NOTED. PERFORMED ADJUST/TEST OF RECIRC SYS IAW MM 21-25-00-5, PASSED. DUE TO WATER INTRUSION IN FWD E/E BAY, R & R STATIC CONVERTER AS PRECAUTION IAW MM 24-33-03-4. REPLACED MAIN BATTERY CHARGER IAW MM 24-31-02-4. SYS GROUND FUNCTION CHECKED GOOD. REINSPECTED ALL AVIONICS & ELECTRICAL AREAS & FOUND NO ODOR, SIGNS OF SMOKE, OR BURNING. A/C FOR SERVICE.

Part: HANDLE — UNSECURE (COCKPIT WINDOW) · airframe 74,118 hrs · 26,178 cycles

COPILOT S WINDOW HANDLE ROTATES OPEN DURING FLIGHT. THE FRONT LATCH STAYS LATCHED, BUT THE HANDLE ROTATES OPEN (HAS TO BE HELD SECURE) AND THE ALIGNMENT ARROWS AT THE AFT END OF THE WINDOW SPLIT APART FROM EACH OTHER. INSPECTED LOCKING MECHANISM OF THE WINDOW AND FOUND OK,FOUND OPERATING MECHANISM CLUTCH NOT PROPERLY ADJUSTED, CRANK ROLLING BY ITSELF. PERFORMED ADJUSTMENT OF WINDOW OPERATING CRANK AND OPERATING MECHANISM CLUTCH AS PER AMM 56-11-02-5.SYSTEM OK. AIRCRAFT OK FOR SERVICE.

Part: NONE — NONE (N/A) · airframe 73,881 hrs · 26,059 cycles

RAMP REPORTED L1 DOOR UNABLE TO BE OPEN FROM OUTSIDE. WHEN IT IS CLOSED WITH OUTSIDE HANDLE, INSIDE HANDLE DO NOT FOLLOW TO COMPLETE CLOSED POSITION. THE INSIDE HANDLE IS WORKING FINE, CLOSING AND OPENING DOOR WITHOUT PROBLEMS. REMOVED HANDLE MECHANISM IAW AMM 52-11-13-2-0 FOR INSPECTION UNTIL STEP 3 E. (1) H, EXTERIOR HANDLE ROTATED FREELY. FOUND SHIM ITEM 17 FIGURE 201 AMM 52-11-13-2 NOT INSTALLED. FOUND WEAR MARK ON CLUTCH COLLAR (18). FOUND ROLLER ON COCKING ROLLER CRANK DAMAGED. REPLACED DAMAGED CLUTCH AND BOTH CAM ROLLERS AND REINSTALLED HANDLE MECHANISM ASSY IAW AMM 52-11-13-2-0. THE TRAVEL OF THE CENTER SHAFT WITHOUT SHIM WAS WITHIN LIMIT AND DON'T NEED SHIM INSTALLATION IAW AMM 52-11-13-2-0.

Part: UNKNOWN — FAULTED (TE FLAPS) · airframe 73,536 hrs · 25,834 cycles

TE FLAPS EICAS WHEN SELECTING FLAPS 1 FOR APPROACH. DUE TO QRH AND CHECKLIST DEMANDS, OPTED TO DISCONTINUE APPROACH. COORDINATED A HOLDING PATTERN AND RAN THE QRH AND ASSOCIATED CHECKLISTS. WERE ABLE TO COMPLETE ALTERNATE FLAPS TO 20 AND LAND NORMALLY. TLV U FIM 27-51 FAULT TREE 808 PERFORMED AND FLAPS OPERATIONAL TEST PERFORMED I.A.W AMM 27-51-00 .SYS IS O.K

Part: FLAP SYSTEM — FAULTED (TE FLAPS) · airframe 73,541 hrs · 25,835 cycles

TE FLAP DISAGREE ON APPROACH. RAN QRH. DECLARED EMERGENCY. LANDED. REPEAT WRITE UP. INTERROGATED FSEU, #1 SHOWS FAULT 305: FLAP ISOL VLV. T/S CONTINUE DURING INSPECTION, FOUND LACK OF LUBRICATION ON L/H AND R/H INBOARD DRIVE OF BOTH INNER FLAP WITH OVERLOAD INDICATIONS TRIPPED. RESET INDICATORS AND LUBRICATED TRACKS, ROLLERS, GIMBALLS AND BALLSCREWS IAW 12-21-09-3. ALSO FOUND OUTBOARD FLAP TRANSMISSION OF BOTH INNER FLAP AND INNER FLAP TRANSMISSION OF BOTH OUTER FLAP WITH IMPROPER OIL LEVEL. SERVICING IN PROGRESS IAW 12-13-06-3. INTERROGATED FSEU, #2 AND #3 NO FAULT FOUND. FOR THE FAULT FAULT "FLAP ISOL VLV" FOLLOWED FIM 27-51 FAULT TREE 818 FIG 113 UNTIL BLOCK 45, UNABLE TO DUPLICATE AFTER SEVERAL CYCLE, NO FAULT ANYMORE. SERVICED OUTBOARD FLAP TRANSMISSION OF BOTH INNER FLAP AND INNER FLAP TRANSMISSION OF BOTH OUTER FLAP IAW AMM 12-13-06-3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,283 hrs · 25,596 cycles

MDIS 974 33-50 7299 18FEB21 MUC OPEN U SEE ALSO 33-50 WRI 7298: EMRGENCY LIGHTS IN CABIN MID AND RIGHT AND RIGHT EXTERIOR DOES NOT ILLUMINATE IN ALL POSITIONS. TROUBLESHOOTING PERFORMED, FOUND NO ILLUMINATION ON RH SIDE. ACC AMM: 33-51-07-2 BATTERY AT POS M730 REMOVED AND REPLACED , FUNCTION CHECK PERFORMED, FOUND OK PART DETAIL ACC GMM 12-7-600: BATTERY,HOLDER ASSY-BATTERY

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS) · airframe 73,283 hrs · 25,596 cycles

MDIS 974 33-50 7298 18FEB21 MUC OPEN U AFTER AIRCRAFT POWER OFF FOUND EMERGENCY LIGHT IN COCKPIT LEFT SIDE ABOVE DOOR AND LEFT EXTERIOR LIGHT ILLUMINATED. WITH AC POWER ON LIGHTS GO OFF . CHECKED AND MOVED EMERG. LIGHT SWITCH IN COCKPIT SEVERAL TIMES TO OFF . NO HELP. WITH AIRCRAFT POWER ON LIGHTS ARE OFF. CHECKED ALL TEST SWITCHES AND ON ARM OF SWITCH FOR FUNCTION , FOUND OK, PERFORMED ALSO SEVERAL POWER SWITCHINGS, APU AND EXTERNAL POWER. FAULT SEARCH ACC WDM33-51-11 PG 926AND WDM 33-51-12 PG 930 PERFORMED. FOUND BATTERY PACK AT M731 POWER SUPPLY NOT CORRECT INSTALLED , SCREWS NOT LOCKED. AFTER BATTERY PACK CORRECT INSTALLATION ACC AMM: 33-51-07-2 . FUNCTION CHECK NORMAL

Part: COLLAR — BROKEN (L1 DOOR) · airframe 72,478 hrs · 25,066 cycles

L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED PANEL 221AL TO GET ACCESS TO COLLAR AS PER MM 52-11-08-4. INSTALLED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. OPS CHECK OK. STILL NEED TO INSTALL THE 221AL PANEL WHICH STILL IN LEAD OFFICE. INSTALLED PANEL 221AL AS PER MM 52-11-08-4. SEALANT APPLIED, OPENED ANOTHER WRI (53-50/6425) TO MONITOR SEALANT CURING. ITEM CLOSED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,359 hrs · 24,946 cycles

LT PASSENGER DOOR EXTERNAL EMERGENCY LIGHT L25 INOP. POWER SUPPLY M731 REPLACED.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 72,220 hrs · 24,812 cycles

PDIS 974 36-10 5902 10SEP19 CDG OPEN U LOGPAGES:3010680 REJECTED TAKEOFF FOR " L ENG BLEED OFF " AFTER ENGINE REDUCED IDLE EICAS MESSAGE REMOVED. GOT EICAS MESSAGE ON SECOND TAKEOFF AND AFTER AIRBORNE RAN QRH AND SELECTED LEFT ENGINE BLEED AIR OFF. PRESSURE GAUGE SHOWS 48 PSI FOR BOTH ENGINES. "MEL 36-11-01: LEFT PRESSURE REGULATING AND SHUTOFF VALVES - INOP CLOSED. A/C MAX FL350. AIRCRAFT RESTRICTED FROM OPERATING INTO KNOWN OR FORECAST ICING CONDITIONS. REFER TO THE OPERATIONS NOTE FOR DRY ICE RESTRICTIONS." *MOCC UPDATE* PLEASE WORK IN CONJUNCTION WITH TSI: 36-10/5903. *THANKS MOCC TECH SERVICES* ACT 11SEP19 15:56 LT PRSOV REPLACED IAW AMM 36-11-09-2-1 TEST PERFORMED ALL PARAMETERS OK IAW AMM 36-11-00-5 OPS CHECK OK.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 72,207 hrs · 24,797 cycles

RH I/B FLAP, LOWER SURFACE REPAIR 52" FORM O/B EDGE AND 13" FORM T/E. REPAIR FOUND TO BE UNSERVICABLE PLEASE PERFORM REPAIR IAW SRM 57-53-01-0I IDENT 1, SRM 57-53-01- 2R REPAIR 1, AND SRM 51-70-10-2R. RH I/B MAIN TRAILING EDGE FLAP REPLACED IAW AMM 27-51-02 DUE TO DISBOND BEING OUTSIDE REPAIR LIMITS,

Part: SKIN — DAMAGED (BS 620-624) · airframe 72,207 hrs · 24,797 cycles

UPON EVALUATION OF AGING AIRCRAFT INSPECTION OF EXISTING DOUBLER AND TRIPLER REPAIR @ BSTA 620-624, STR21R - STR24R DAMAGED FASTENER HOLE FOUND ON INTERNAL SKIN WORK INSTRUCTIONS CARRIED OUT IAW FEDEX E.A.#F-5330-T0348760 TITLE: AD 2006-11-11 - FUSELAGE - PLATES & SKINS - MISDRILLED HOLE @ EXISTING REPAIR STA 620

Part: PANEL — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 72,207 hrs · 24,797 cycles

NR 2 ENG I/B C-DUCT UPPER BIFURICATION PANEL DAMAGE UPPER BIFURICATION UPPER TRACK BEAM SUPPORT PANEL EVALUATED AND FOUND TO BE CORROSION. CORROSION OUT OF LIMITS AS PER EM 78-31-28-300-085 REPLACED THE THRUST REVERSER ASSY IAW W/O:00074899 WRI:78305814 AND SEQ # 000623.

Part: NOZZLE — CRACKED (NR 1 ENG EXHAUST) · airframe 72,207 hrs · 24,797 cycles

NR 1 ENGINE CNA HAS CRACKS AT THE 3 O'CLOCK AND 9 O'CLOCK POSITIONS. CRACKS REMOVED IAW EM 78-11-04 AND CRACKS REPAIR IAW E.A. F-7810-T0348465.

Part: PANEL — CRACKED (RT WING SLAT) · airframe 72,207 hrs · 24,797 cycles

SLAT #6 IN/B T/E SKIRT (FLEX PANEL) IS CRACKED. REPAIRED CRACK IAW SRM 51-70-17 GENERAL & E.A. F-5750-T0348677

Part: SKIN — DENTED (BS 580-597) · airframe 72,207 hrs · 24,797 cycles

DENT OUTSIDE PERMITTED LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE FIG101 DETAIL III @ B/S 580-597 STR 25L REAPIRED DENT IAW FEDEX EA# F-5300-T0348400 (P1) AND SRM 51-00-01 REPAIR 28 FIG 1

Part: STRINGER CLIP — CRACKED (BS 1500) · airframe 72,207 hrs · 24,797 cycles

STRINGER CLIP ' B/S 1500 STR2 WAS FOUND DAMAGED AND CRACKED . REPLACED STRINGER CLIP IAW SRM 51-40-02

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 72,207 hrs · 24,797 cycles

SEAT TRACK B/S 364 RBL 47-51 CORRODED BEYOND PERMITTED LIMITS. REPAIRED IAW FEDEX EA F-5310-T0348507(P1).

Part: FLOOR SUPPORT — NONE · airframe 72,207 hrs · 24,797 cycles

EXISTING REPAIR FOUND ON FLOOR SUPPORT STRUCTURE BS 570 APPROX. LBL 10. REPAIR REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA EVALUATION CARRIED OUT OF EXISTING REPAIR ON FLOOR SUPPORT STRUCTURE AT BS.570 APPROX LBL.10 IAW FEDEX EO F-5100-7-5001 PART 1 ATTACHMENT B AND ON VISUAL INSPECTION AND SRM REVIEW, THE REPAIR LAYOUT AT BS 570 APPROX LBL 10 WAS IDENTIFIED AS CONFORMING TO SRM REPAIR 53-00-53-2R REPAIR 1, THIS IS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 72,207 hrs · 24,797 cycles

FLOORBOARD @ 1L DOORWAY DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 72,207 hrs · 24,797 cycles

FLOOR PANEL DAMAGED @ DOORWAY #1R OUTSIDE PERMITTED LIMITS IAW SRM53-00-50-1A REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R

Part: STRAP — CRACKED (GALLEY FLOOR) · airframe 72,207 hrs · 24,797 cycles

STRAP CRACKED FWD GALLEY FLOOR BS 367 ,LBL 24 FABRICATED NEW STRAP AND REPLACED OLD PART IAW EA F-5310-T034848 PART 1, SRM 53-00-5-2R, REPAIR 13, AND GMM. 7-0-1001.

Part: SEAT TRACK — CORRODED (BS 344-377) · corrosion level 2 · airframe 72,207 hrs · 24,797 cycles

SEAT TRACK HAS EVIDENCE OF CORROSION @ B/S-344-356 AND 367-374. REMOVED SEAT TRACK SECTION IAW SRM 51-40-02. REMOVED CORROSION FROM SEAT TRACK SECTION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG101 DETAIL 1. MATERIAL REMOVED 0.060" MAX ALLOWABLE 0.040" FABRICATED NEW SEAT TRACK IAW DOCUMENT #3504-NC-2 AND GMM 7-0- 1001. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DRAWING # 3470.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 72,185 hrs · 24,779 cycles

PDIS 974 27-50 5786 08JUL19 TLV OPEN U LOGPAGES:3010096 TE FLAP ASYM INDICATED WHEN FLAPS SELECTED TO "1". FOLLOWED QRH PROCEDURES TO LANDING. TOUCHDOWN SPEED WAS APPROX 170 KIAS. FIM 27-51 TREE 805 PERFOMED NO FINDINGS, FLAPS SYS OPER TEST PERFORMED SEVERAL TIMES IAW AMM 27-51-00-715-149 FOUND OPERTATION OK AND NO MSG APPEARED.

Part: BULB — INOPERATIVE (L1 DOOR SLIDE) · airframe 71,875 hrs · 24,484 cycles

EMERGENCY SLIDE LIGHT L1 NO LIGHT FACT 03FEB19 11:23 CPH EMERGENCY SLIDE LIGHT L1 BULP REPLACED AMM 33-51-06-2-1 REV 123.4 BULP P/N 767 LIGHT TEST PERFORMED NO REMARKS

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 71,188 hrs · 23,616 cycles

COMPOSITE DISBOND TOP OF LEFT OUTBOARD AFT FLAP. REPAIRED AREA AT TOP OF LEFT OTBD AFT FLAP IAW SRM 57-53-01-2R, FIG 201, TABLE II, AND SRM 51-70-04, PAR 5.A.1. TAP TESTED AREA IAW 51-10-06 WITH NO DEFECTS NOTED. PRIMED AND TOPCOATED AREA IAW SRM 51-20-01 AND AMM 51-21-10.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,998 hrs · 23,495 cycles

FOUND ON PREDEPARTURE CHECK, 2 EA EMERGENCY EXIT SIGNS AND RT EXTERIOR LIGHT NOT TESTING. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK PER AMM 33-51-07-2, OPS CHECKS NORMAL.

Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 70,993 hrs · 23,488 cycles

L1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT L1 DOOR ESCAPE SLIDE POUCH REF: 757 M.M. 52-11-02-4

Part: PIN — MISSING (R1 DOOR SLIDE) · airframe 70,993 hrs · 23,488 cycles

R1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT R1 DOOR ESCAPE SLIDE POUCH IAW MM 52-11-02-4.

Part: SKIN — DAMAGED (RUDDER) · airframe 70,573 hrs · 23,186 cycles

RUDDER HAS HAIL DAMAGE. ACCOMPLISHED 3 EA REPAIRS ON RUDDER LT SIDE IAW SRM 55-40-01-2R, 51-70-04-0G AND EA F05540-T0328008, P1 TRACKING REPAIRS.

Part: SKIN — DENTED (CARGO DOOR) · airframe 70,573 hrs · 23,186 cycles

DENTS IN MAIN CARGO DOOR SKIN. EVALUATED AND MEASURED DENTS, 224, MAIN CARGO DOOR SKIN, HFEC AND DVI INPSECTIONS CW, NO ADDITIONAL DEFECTS NOTED. DENTS, 195, FOUND TO BE WITHIN LIMITS IAW EA F-5230-TO327693 PT 1 AND DENTS, 43-55, 103-120, 29 TOTAL. REPAIRED IAW EA F-5230-TO327693 PT1.

Part: PROXIMITY SENSOR — FAILED (R1 DOOR SLIDE) · airframe 70,202 hrs · 22,903 cycles

SLIDE LIGHT IN DOOR R1 FAILS TO ILLUMINATE WITH DOOR ARMED. R1 ESCAPE SLIDE ARMED INDICATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 DOOR AFT SLIDE PROXIMITY SENSOR IAW AMM 25-66-11-2. OPS CHECKED GOOD .

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 697 hrs · 22,591 cycles

BS 415, LBL 54 DECK PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED DOUBLER REPAIR & INSTALLATION IAW SRM 757-200 RIGID CARGO BARRIER SECTION 5 4 3.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 696 hrs · 22,499 cycles

RIGHT SIDE ENTRY DOOR WOULD NOT ARM. FOUND GIRT BAR ARMING LANYARD WRAPPED AROUND GIRT BAR. R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. INSPECTED THE SLIDE UPON ARRIVAL, SLIDE WAS REMOVED AT PREVIOUS STATION. LANYARD IS IN A DISARRAY & UNSURE HOW IT'S SUPPOSED TO BE PLACED IN THE SLIDE. ORDERING A NEW SLIDE. WILL REQUIRE A RII FOR INSTALLATION. REPLACE R1 SLIDE ASSEMBLY IAW AMM 25-66-01-4.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 69,368 hrs · 22,274 cycles

UPON LANDING, DOOR ARM LIGHT DOOR 1R WAS NOT ILLUMINATED. RELAMPED, NO HELP. FOUND SOME DEBRIS AT GIRT BAR AFT HOOK. REMOVED DEBRIS, LIGHT NOW OPERATES WHEN DOOR IS ARMED.

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 69,339 hrs · 22,257 cycles

ON BLOCK OUT R2 DOOR WOULD NOT ARM & ARM LIGHT WOULD NOT LIGHT. FOUND ESCAPE SLIDE GIRT BAR FELL OUT OF PLACE & WAS ABLE TO PLACE BACK IN PLACE. TESTED IAW MM 52-11-25-5 & NOW ARMS GOOD & IS GOOD FOR SERVICE.

Part: LANYARD — OUT OF POSITION (ENTRY DOOR) · airframe 68,982 hrs · 22,008 cycles

RIGHT FWD ENTRY DOOR WILL NOT ARM DOOR SLIDES INOPERATIVE. NO JUMPSEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. FOUND CORD OF SLIDE TANGLED IN BAR. NO TIME OR RII TO REMOVE & FIX. FOUND STATIC LANYARD LINE CLIP LAYING BETWEEN GIRT BAR CAM & FLOOR FITTING. REMOVED LANYARD & STOWED IN SLIDE BAG. OPERATIONS CHECKED GOOD IAW OK FOR SERVICE.

Part: SLIDE RAFT — DEPLOYED (L1 DOOR) · airframe 68,500 hrs · 21,665 cycles

L1 MAIN CABIN EXIT SLIDE DEPLOYED. RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 10DEC13 MEL 52-11-01-A L1 DOOR SLIDE MISSING IDENTIFY INOPERATIVE OR MISSING. ADDED MPN D30654-122 CPN 2520951 QTY 1 SLIDE UPDT 07DEC13 19:01 GJT R AWAITING SLIDE ASSY. MC1 R MEL EXTENSION GRANTED FOR 1 DAY NEW EXPERATION DATE IS DEC 10 2013. ATTEMPTED TO INSTALL A NEW ESCAPE SLIDE, L1 DOOR POSITION. HAD TROUBLE GETTING THE GIRT BAR TO PROPERLY INSTALL PER M/M 26-66-01-4. RAN OUT OF TIME DUE TO NEEDING TO PREFLIGHT & DEICE THE JET. REMOVED THE NEW ESCAPE SLIDE SINCE IT WAS NOT FULLY INSTALLED.REINSTALLED COVER PER M/M 25-66-01-4. INSTALLED A NEW PASSENGER DOOR EMERGENCY POWER RESERVOIR BOTTLE UNDER WRI 52-20-0764. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IN REF TO B757 AMM CH 25-66-01-4, OPS CHECKS NORMAL. PREMATURE REMOVAL/INSTALLATION OFF MFG D30654-122.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,300 hrs · 21,511 cycles

EMERGENCY LIGHTS R1 DOOR EXTERIOR SLIDE INOPERATIVE. REPLACED LAMPS, OPS NORMAL, IAW AMM 33-51-06-2-1. OK FOR SERVICE.

Part: TEE FITTING — CRACKED (WNG-BDY FAIRING) · airframe 68,268 hrs · 21,498 cycles

LOWER FUSELAGE BS 900 - 1037, LBL 60 WING TO BODY FAIRING SUPPORT TEE CRACKED AT AFT INBD CORNER. REPAIRED IAW EA F-5310-167523 PART 1.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

CABIN FLOORBEAM BS 1640 RBL 24 CORRODED. R & R WITH FLOORBEAM FABRICATED IAW DWG 146N5136, SHT 1 REV - AND INSTALLED IAW DWG 146N5089, SHT 6, REV. MAJOR REPAIR.

Part: PANEL — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

RIGHT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 92.5, FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. REPAIR IS MAJOR.

Part: PANEL — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

RT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 81.0 FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. MAJOR REPAIR.

Part: WEB — CORRODED (R4 DOOR) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

R4 DOOR INTERNAL DOOR HANDLE MECHANISM CUTOUT FWD INTERCOSTAL FWD SIDE FOUND CORRODED. REMOVED AND REPLACED, FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV.H. REPAIR IS MAJOR.

Part: WEB — CORRODED (R4 DOOR) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

R4 DOOR INTERNAL DOOR-MOUNTED WINDOW CUTOUT FWD WEB FWD SIDE HAD MINOR CORROSION. REMOVED AND REPLACED FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV.H. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1000-1010) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1000 -1010 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND FASTENER HOLES. REPAIRED.

Part: CREASE BEAM — CHAFED (BS 1016) · airframe 68,268 hrs · 21,498 cycles

BS 1016 RT CREASE BEAM INBD ANGLE FOUND CHAFED. REPAIRED IAW REPAIR DWG LOR5L53017 SHT.3, REV A. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 960-980) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 960-980 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND THREE FASTENERS HOLES. REPAIRED IAW REPAIR DWG LOR5L53017 SHT 3, REV A. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

SEAT TRACK AT BS 365, RBL 24.75, FOUND CORRODED ON LT AND RT TRACK FLANGE. SEAT TRACK REMOVED IAW SRM 51-40-02 REV.109 AND INSTALLED NEW IAW DWG 141N5130 SHT.1. REV. F. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1260-1270, RT CREASE BEAM INBD ANGLE HAS THREE AREAS OF HEAVY CORROSION. REPAIRED IAW EA F-5310-167516, PART 1. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

FUSELAGE SKIN RT SIDE MISREPAIRED AT BS 600-620, FROM STR 27R- 27L. REPAIRED IAW SRM 53- 00-01 FIG.201, REPAIR 9, DETAIL II, REV.109. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

FUSELAGE SKIN HAS NUMEROUS NICKS AND SCRATCHES BETWEEN STRINGER 26L AND 26R AT BS 540 TO 560. REPAIRED IAW EA F-5330-167512, PART 1. REPAIR IS MINOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 980 -1000 RT CREASE BEAM FOUND CORRODED AROUND SIX FASTENER HOLES. REPAIRED IAW REPAIR DWG LOR5L53017 SHT 3, REV A. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1380 -1400, RT CREASE BEAM OTBD ANGLE FOUND CORRODED. REPAIRED IAW EA F-5310-167509, PART 1. REPAIR IS CAT B, MAJOR.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

AFT CARGO DOOR HAS CORROSION AT ATTACHMENT OF SNAP FASTENER AT FWD SIDE FRAME WEB. REPAIRED IAW EA F-5230-166076 PART 1. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1620) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

SEAT TRACK AT BS 1620, LBL 45.5, FOUND WITH CORROSION ON THE BOTTOM PORTION OF TRACK. REPAIRED IAW SRM 53-00-52, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 794, RBL 45.5, SEAT TRACK CROWN FOUND CHAFED. REPAIRED IAW SRM 53-00-52 FIG.201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

SEAT TRACK FLANGE, RT SIDE UPPER SURFACE AT 1320 LBL 24.75 FOUND WITH MINOR CORROSION. REPAIRED IAW 53-00-52, FIG 201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (BS 1594-1599) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1594-1599, RBL 45.5 SEAT TRACK FLANGE FITTING FOUND CORRODED. REPAIRED IAW SRM 53-00-02 FIG 201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (BS 1594-1599) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1594-1599, RBL 45.5 SEAT TRACK FLANGE FITTING FOUND CORRODED. REPAIRED IAW SRM 53-00-02 FIG 201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

SEAT TRACK AT BS 1580-1610, LBL 45.5 FOUND CORRODED AT THE BOTTOM PORTION OF TRACK. REPAIR CARRIED OUT ON SEAT TRACK SECTION IAW SRM 53-00-52, FIG 201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SKIN — GOUGED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

FUSELAGE EXTERIOR SKIN GOUGEED AT BS 620 - 624 S21-24R. REPAIRED IAW EA F-5330-166079, PART 1. CAT B, MAJOR REPAIR.

Part: FLOORBEAM — CHAFED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

BS 324 LBL 24-62 FLOORBEAM UPPER TEE FOUND CHAFED. DAMAGE REMOVED IAW SRM 51-10-02, REV 108, FOUND WITHIN LIMITS OF SRM 53-10-08. ALLOWABLE DAMAGE 1, FIG 101, REV 108. REPAIR IS MINOR.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 68,268 hrs · 21,498 cycles

BS 324, BL0 -RBL 5 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, REV 108. FOUND WITHIN LIMITS OF SRM 53-10-08 ALLOWABLE DAMAGE 1, FIG 101, REV 108. REPAIR IS MINOR.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

R4 DOOR UPPER HINGE CUTOUT INTERNAL AREAS FOUND CORRODED. R & R WEB, FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV H. REPAIR IS MAJOR.

Part: WEB — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

CABIN BS 1340-1350 R3 DOOR LOWER MAIN WEB SILL LOWER SURFACE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, REV 109. FOUND EXCEED LIMITS WITH NO SRM ALLOWABLE DAMAGE. WEB REMOVED IAW SRM 51-40-02, REV 109. NEW WEB FABRICATED IAW DWG 146N8326, SHT 1, REV C AND INSTALLED IAW DWG 146N8322, SHT 1, REV F. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

FUSELAGE EXTERIOR SKIN LT SIDE CORRODED BS 704, 1 INCH ABOVE STR 25L. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 108. REPAIR IS CAT B, MAJOR.

Part: FRAME — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1280, STR 11-12R FRAME INBD EDGE FOUND CHAFED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3 REV 108. REPAIR IS CAT B MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1020-1040, RT CREASE BEAM WEB UPPER SURFACE FOUND CORRODED. R & R IAW DWG 144N5140, SHT 2, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1560-1640, RBL 45.5 SEAT TRACK FOUND MINOR CHAFE ON SEAT TRACK CROWN, CENTER BOTTOM OF CROWN.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

CABIN SEAT TRACK AT BS 1440-1490, LBL 24.75 FOUND MULTIPLE CHAFED AT SEVERAL LOCATIONS ON CROWN AREA. REPAIRED IAW SRM 53-00-52, FIG 201, OPTION 1, REPAIR 1, REV 109. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 365-377, RBL 24.75, SEAT TRACK CORRODED. R & R WITH NEW SEAT TRACK SUPPORT IAW DWG 141N5130 SHT 1, REV F. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 324, RBL 38-60, FLOORBEAM UPPER TEE SURFACE FOUND CORRODED. REPAIRED IAW EA F-5310-168316. MAJOR REPAIR.

Part: SILL — CORRODED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

AFT CARGO BAY DOOR LOWER SILL FOUND CORRODED BS 1440 - 1460. R & R WITH NEW WEB FABRICATED AND INSTALLED IAW DWG 146N8522, SHT 1 REV E. REPAIR IS MAJOR.

Part: ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

FUSELAGE RT SIDE INTERIOR BS 1790 -1792 AT STR 6 THE SMALL ANGLE THAT HOLDS THE APU INLET HAS CORROSION. ANGLE R & R IAW DWG 148N3105, SHT.1 REV C. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1172) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1172 RT CREASE BEAM WEB UPPER SURFACE FOUND CORRODED. R & R WITH NEW SHEAR WEB, FABRICATED IAW DWG 144N5210 SHT1, REV.- AND INSTALLED IAW DWG 144N5200, SHT.2, REV B. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 740-760, RT CREASE BEAM INBD ANGLE LOWER SURFACE FOUND CORROSION AT BS 750. CORROSION REMOVED IAW SRM 51-10-02, REV 109. FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-15, FIG 101, DAMAGE 1, REV 109. REPAIR IS MINOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 377.7, BL 0- RBL 54 FLOORBEAM UPPER TEE SURFACE FOUND CORRODED. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5123, SHT.1 REV A AND INSTALLED IAW DWG141N5113, SHT 1, REV F. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 345, BL 0-LBL 20 FLOORBEAM UPPER TEE AND LOWER SURFACES FOUND CORRODED. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5121, SHT 4, REV AND INSTALLED IAW DWG 141N5111, SHT 1, REV C. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 365, RBL45-60 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORROSION. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5122, SHT.1, REV A AND INSTALLED IAW DWG 141N5112 SHT.1, REV D. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 365, RBL 55-60, FLOORBEAM UPPER TEE LOWER SURFACE FOUND CORRODED. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5122, SHT.1, REV A AND INSTALLED IAW DWG 141N5112 SHT 1. REV D REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 365, BL 0-RBL 24 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORRODED. R & R WITH NEW FLOORBEAM, FABRICATED IAW DWG 141N5122, SHT.1, REV A AND INSTALLED IAW DWG 141N5112, SHT 1, REV D. REPAIR IS MAJOR.

Part: FRAME — CHAFED (BS 1280) · airframe 68,268 hrs · 21,498 cycles

BS 1280, FRAME FOUND CHAFED JUST BETWEEN S10-14L. REMOVED DAMAGE IAW SRM 51-10-02, REV 109 AND FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-07. ALLOWABLE DAMAGE 2, FIG 101, REV 109. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3, REV 109. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1661, RBL 40-50 FLOORBEAM TEE UPPER SURFACE FOUND CORRODED. FLOORBEAM FABRICATED IAW DWG 146N5110, SHT 2 REV B AND INSTALLED IAW DWG 146N5090, SHT 5, REV. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 345 BL 0-RBL 15, FLOORBEAM UPPER TEE SURFACE CORRODED. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5121, SHT 4 REV AND INSTALLED IAW DWG 141N5111, SHT 1, REV C. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 365 LBL 44-46 FLOORBEAM UPPER TEE LOWER SURFACE FOUND MINOR CORROSION AROUND FASTENER HOLE. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5122, SHT 1, REV A AND INSTALLED IAW DWG 141N5112 SHT 1, REV D. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 365, RBL 10-14 FLOORBEAM UPPER TEE LOWER SURFACE FOUND CORRODED. R & R FLOORBEAM, FABRICATED IAW DWG 141N5122, SHT 1 REV A AND INSTALLED IAW DWG 141N5112, SHT 1 REV.D. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1661, RBL 56 FLOORBEAM UPPER TEE FOUND CORRODED. R & R FLOORBEAM FABRICATED IAW DWG 146N5110, SHT 2, REV B AND INSTALLED IAW DWG 146N5090, SHT 5, REV. REPAIR IS MAJOR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

FLOORBEAM AT BS 345, LBL 48 DAMAGED. R & R WITH NEW FLOORBEAM FABRICATED IAW DWG 141N5121, SHT 4 REV AND INSTALLED IAW DWG 141N5111, SHT 1, REV C. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 377.7, BL 0-RBL 24 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORRODED. R & R FLOORBEAM, FABRICATED IAW DWG 141N5123, SHT 1, REV A AND INSTALLED IAW DWG 141N5113, SHT 1, REV F. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1661, BL 0-LBL 24, FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORRODED. FLOORBEAM FABRICATED IAW DWG 146N5110, SH 2 REV B AND INSTALLED IAW DWG 146N5090, SHT 5 REV- . REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1661 BL 0-RBL 24, FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORRODED. FLOORBEAM FABRICATED IAW DWG 146N5110, SHT 2 REV B AND INSTALLED IAW DWG 146N5090 SHT 5, REV. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1661, LBL 45- 60 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORROSION. R & R FLOORBEAM FABRICATED IAW DWG 146N5110, SHT 2, REV B AND INSTALLED IAW DWG 146N5090, SHT 5, REV -REPAIR IS MAJOR.

Part: FRAME — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 395, FRAME INBD EDGE FOUND CHAFED BETWEEN STR 15-16R. DAMAGE REMOVED IAW SRM 51-10-02, REV 109, FOUND WITHIN LIMITS OF SRM 53-00-07 ALLOWABLE DAMAGE 2, FIG 101, REV 109. REPAIR IS MINOR.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

BS 1280 FRAME FOUND CORROSION JUST BETWEEN STR 15L-16L.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

CABIN BS 1620, S16-17L, FRAME INBD EDGE FOUND CORRODED. REPAIRED IAW SRM 51-10-02, REV 108 AND STA EA 757-5362-08-E2214, REV.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

MAIN DECK BS 1100 STR 16-17L FRAME WEB INBD EDGE CORROSION. REPAIRED IAW EA F-5310-168326. MINOR REPAIR.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,268 hrs · 21,498 cycles

MAIN DECK BS 1160, FRAME WEB INBD EDGE CORROSION BETWEEN S16-17R. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4, REV 109. REPAIR IS CAT B, MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

FUSELAGE SKIN, NUMEROUS SMALL SCRATCHES ALONG THE PERIMETER OF THE WING TO BODY FAIRING MATING SURFACE AT BS 780-800, STR 17 - 19R. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 109 AND EA F-5330-T0300676, PART 1. REPAIR IS CAT B, MAJOR.

Part: FLOORBEAM — SCRATCHED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

CABIN FLOORBEAM AT BS 1240, LBL 30 FOUND WITH SCRATCHES. REPAIRED FLOORBEAM IAW EA 757-5365-08-E2211, REV A.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

CABIN FLOORBEAM AT BS 1240, BL 0 - LBL 24.75 FOUND MULTIPLE SCRATCHES. REPAIRED IAW EA 757-5365-08-E2211, REV A.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 800 RBL 60 - 65 FLOORBEAM UPPER TEE FOUND WITH MINOR CORROSION. REPAIRED IAW EA F-5310-168329.

Part: FRAME — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1640 FRAME INBD EDGE FOUND CORRODED BETWEEN S5 - 6L. REPAIRED IAW STA EA 757-5362-08-E2225, REV.

Part: FLOORBEAM — CHAFED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1640, RBL 39 FLOORBEAM UPPER TEE CHAFED. R & R FLOORBEAM FABRICATED IAW DWG 146N5109, SHT 1, REV A AND INSTALLED IAW DWG 146N5089 SHT 7, REV. REPAIR IS MAJOR.

Part: FRAME — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1681 FRAME FOUND CORRODED AT S5L. REPAIRED IAW SRM 51-10-02, REV 108 AND STAE EA 757-5362-08-E2226, REV-.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1640 RBL 50- 60 FLOORBEAM UPPER TEE CORRODED. R & R FLOORBEAM FABRICATED IAW DWG 146N5109, SHT 1, REV A AND INSTALLED IAW DWG 146N5089, SHT 7 REV. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,268 hrs · 21,498 cycles

BS 1640, LBL 45 - 60 FLOORBEAM UPPER TEE FOUND CORRODED AROUND FASTENER HOLES. R & R WITH NEW BEAM FABRICATED IAW DWG 146N5109, SHT 1, REV A AND INSTALLED DWG 146N5089, SHT 7, REV. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,268 hrs · 21,498 cycles

FUSELAGE SKIN HAD NUMBEROUS NICKS AND SCRATCHES BETWEEN STR 26L AND 26R AT BS 1560 -1580. REPAIRED IAW EA F-5330-T0300813, PART 1. REPAIR IS CAT B, MAJOR.