N718EV

Part: FLOOR SUPPORT — CORRODED (BS 565-693) · airframe 37,287 hrs · 26,838 cycles

LBL 9 T-CAP CORRODED NEEDS TO BE REPLACED FROM FS565.00 THRU FS693.00. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED LBL 9 FLOOR BEAM T-CAP FROM FS-565.00 THRU FS-693.00 IAW CRJ-700 REO-670-53-31-631,SRM53-00-41-201-001-A01,NDTM-51-20-006-250,AMM-26-17-01,AMM-26-10-00,SRM-51-25-16-001-A01.

Part: FAIRING — CRACKED (BS 909 S24R) · airframe 37,287 hrs · 26,838 cycles

SUPPORT STRUCTURE FOR FAIRING 196AR CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24RH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER 670-53-82-575. FORM M-337 COMPLETED.

Part: FAIRING — CRACKED (BS 909) · airframe 37,287 hrs · 26,838 cycles

SUPPORT STRUCTURE FOR FAIRING 195AL CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24LH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER 670-53-82-575. FORM M-337 COMPLETED.

Part: FRAME — CRACKED (BS 333 S0-S1R) · airframe 37,287 hrs · 26,838 cycles

POSSIBLE CRACK AT FRAME FS333 BETWEEN STR0 AND STR1 R/H. (C-CHECK RO 4/20/2021) PERFORMED REPAIR IAW REO 670-53-21-1954, SEE ATTACHED FORM M-337.

Part: CHANNEL — CORRODED (BS 1035-1045) · airframe 37,287 hrs · 26,838 cycles

FS 1035 TO1045 DOUBLER AND DOME NUTS BETWEEN STR. 27R AND 26R NEEDS CLEANED AND EVALUATED (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED INNER NUT PLATE CHANNEL AT FS1035 TO FS1045, STR27R AND STR26R AT AFT DRAIN MAST IAW CRJ700 SRM 51-40-11, 51-42-06, 51-45-00, 51-25-06, 51-41-02, 51-23-00 AND 51-25-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,287 hrs · 26,838 cycles

RIGHT FUSELAGE DENT INSIDE RVSM AREA, LOWER FORWARD BELOW RIGHT TRU DOOR CUT OUT (C-CHECK RO 4/20/2021) COMPLIED WITH REWORK ON DENT ON ADG SKIN PANEL BETWEEN FS185.00 AND FS 193.00 AND STRINGER 16R AND 17R IAW MHIRJ REPAIR ENGINEERING ORDER 670-53-11-1666 AND BOMBARDIER REPAIR ENGINEERING ORDER 670-51-00-085. RVSM MEASURMENTS PERFORMED ON CAMP 22461669

Part: ANCHOR FITTING — CORRODED (BS 533-581) · airframe 37,287 hrs · 26,838 cycles

CORROSION ON TOP SURFACE OF FORWARD CARGO NETTING ANCHOR HOLD DOWNS FS533.00 AND FS581.00. BOTH BETWEEN STRINGERS 23LH AND 22LH. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED FWD CARGO FWD ANCHOR FITTING P/N SH670-33390-1 IAW CRJ700 SRM 51-42-21 AND 51-45-00. BLENDED OUT CORROSION, FOR MATERIAL REMAINIG MEASUREMENTS REFER TO REO # 670-53-32-082 PAGE 3 FIGURE 4, ACCOMPLISHED REWORK ON FWD CARGO AFT ANCHOR FITTING IAW MHIRJ REO # 670-53-32-082.

Part: DOUBLER — CORRODED (BS 985 S26L/R) · airframe 37,287 hrs · 26,838 cycles

CORROSION FOUND ON EXTERNAL DOUBLER @ FS 985.00 STGR 26R TO 26L (C-CHECK RO 4/20/2021) REMOVED CORRODED DOUBLER AND TRIPLER FROM F.S. 985.00 STR 26R TO STR26L IAW CRJ700 SRM 51-42-21. FABRICATED NEW DOUBLER AND TRIPLER FROM .063 2024-T3 P.O.# 7992 IAW BOMBARDIER REO# 670-53-61-722. LOCATED AND DRILLED NEW DOUBLER AND TRIPL,ER IAW BOMBARDIER REO# 670-53-61-722 AND CRJ700 SRM 51-40-11. TREATED AND PRIMED NEW DOUBLER AND TRIPLER IAW INSTALLED NEW DOUBLER AND TRIPLER IAW BOMBARDIER REO# 670-53-61-722 AND CRJ700 SRM 51-42-21

Part: STRINGER — CORRODED (BS 319-349 S22R) · airframe 37,287 hrs · 26,838 cycles

FOUND CORROSION ON STGR 22R AND SPLICE ANGLES @ FS 319.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED STR22R FROM FS319 TO FS349 IAW CRJ700 SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-06 AND 51-25-16.

Part: STRINGER — CORRODED (BS 310-349 S21R) · airframe 37,287 hrs · 26,838 cycles

FOUND CORROSION ON STGR 21R AND SPLICE ANGLES @ FS 310.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED SRT 21R/H P/N SH670-31383-1S FROM FS310- FS349 IAW CRJ700 SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-06 AND 51-25-16.

Part: STRINGER — CORRODED (BS 316 S20R) · airframe 37,287 hrs · 26,838 cycles

FOUND CORROSION ON STGR 20R @ FS 316.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED STR20R/H FROM FS280 TO FS 319 IAW CRJ700 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (BS 310-319 S21L) · airframe 37,287 hrs · 26,838 cycles

STRINGER 21 LEFT CORREDED BETWEEN FS 310.00 TO FS 319.00. GROUNDING POINTS ON FRAME GS 405 AND GS 445 ARE ALSO CORRODED. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED INTERCOSTAL AT STR21L FROM FS 310 TO FS333 IAW CRJ700 SRM 53-21-23, 51-42-06,51-42-20, 51-40-11, 51-24-16,51-24-21 AND 51-24-36.

Part: FRAME — CORRODED (BS 517 S24-26R) · airframe 37,287 hrs · 26,838 cycles

CORROSION AT FS 517.00 LOWER FRAME BETWEEN STRINGERS 26LH AND 24RH. (C-CHECK RO 4/20/2021) REMOVED CORRODED LOWER FRAMES AT FS517 L/H AND R/H, FABRICATED AND INSTALLED NEW LOWER FRAMES FOR FS517, L/H P/N SH670-33261-7 AND R/H P/N SH670-33210-5 IAW BOMBADIER DRAWING SH670-33210, CRJ700 SRM 51-21-16, 51-24-16, 51-24-36, 51-24-06, 51-31-00, 51-40-11 AND CRJ700 NDTM 51-20-006.

Part: BOX BEAM — CORRODED (BS 533-549) · airframe 37,287 hrs · 26,838 cycles

CORRISION INSIDE OF BOX FRAME ABOVE FWD CARGO DOOR, BETWEEN STR 18 AND 19, F/S 533.00 AND 549.00 (C-CHECK RO 4/20/2021) REPAIRED FWD CARGO DOOR LINTEL DAMAGE AT L/H FS533 TO FS549 BETWEEN STR18L TO STR19L IAW MHIRJ REO # SH670-53-31-604.

Part: FRAME — CORRODED (BS 379 S20-22R) · airframe 37,287 hrs · 26,838 cycles

FS 379.00 FRAME CORRODED BETWEEN STRINGER 22RH AND 20RH. FORWARD OF LAVATORY DRAIN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED FRAME FS379 FROM STR26R TO STR20R P/N SH670-32118-1 PO# 00013534R IAW CRJ700 SRM 51-40-11, 51-42-06 AND 51-42-20.

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 37,287 hrs · 26,838 cycles

FILIFORM CORROSION AND ALUMINUM OXIDE ON THE UPPER SURFACE OF THE INBOARD FLANGE OF THE LOWER SILL OF THE AFT BAGGAGE DOOR FRAME WHERE THE FLOORBOARD OUTBOARD EDGE ATTACHES, BETWEEN FS1000 AND FS1047. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED LOWER SILL OF AFT CARGO DOOR IAW CRJ700 SRM 51-40-11, 51-21-06, 51-42-06, 51-42-21, 51-42-13, 51-25-06, 51-25-16 AND BOMBARDIER DWG #MM670-35670.

Part: STRINGER — CORRODED (BS 942) · airframe 37,287 hrs · 26,838 cycles

WING TO BODY FUSELAGE STRINGER @ FS 942.0 HAS CORROSION (C-CHECK RO 4/20/2021) REMOVED DAMAGED ANGLES AND INSTALLED NEW L/H, R/H AND CENTER ANGLES AT WING TO BODY FUSELAGE STRINGER F.S 942.00 IAW CRJ 700 SRM 51-42-O6

Part: SEAT TRACK — DAMAGED (BS 810) · airframe 37,287 hrs · 26,838 cycles

RT SIDE SEAT RAIL FS810 NEEDS CLEANING AND EVALUATIONING ( FLAGGED DOT 402 ) (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RH SEAT RAIL AT FS 785.15 THRU FS853.00 UTILIZING PN 20276 PO# 00013626 IAW CRJ700 SRM 51-40-11, 51-42-02 AND AMM 53-00-49

Part: SEAT TRACK — DAMAGED (BS 785) · airframe 37,287 hrs · 26,838 cycles

RT SIDE SEAT RAIL FS 785.15 NEED TO BE CLEANED AND EVALUATED ALSO MISSING 2EA FASTENERS ( FLAGGED DOT 401 ) (C-CHECK RO 4/20/2021) REMOVED DAMAGED RH SIDE SEAT TRACK AND INSTALLED NEW SEAT TRACK P.O. 00013626 PER CRJ700 AMM 53-00-49

Part: VANE — WORN (RT WING TE FLAP) · airframe 37,287 hrs · 26,838 cycles

RIGHT HAND FLAP VANE STOPPER IN THE WING TRAILING EDGE- CENTER AND I/B STOPPER PADS MISSING O/B PAD WORN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RIGHT WING INBD FLAP VANE STOPS CENTER, INBD, OUTBD IAW CRJ 700 SRM 57-51-02

Part: VANE — WORN (LT WING TE FLAP) · airframe 37,287 hrs · 26,838 cycles

LH I/B FLAP VANE STOPPERS IN THE WING TRAILING EDGE- O/B STOPPER PAD WORN AND CENTER AND I/B STOPPER PAD MISSING. (C-CHECK RO 4/20/2021) LH FLAP - REPLACED CENTER & OUTBOARD STOPPERS (CC670-16073). REPLACED INBOARD STOPPER (CC670-16022). I.A.W. 57-51-02

Part: INTERCOSTAL — CORRODED (BS 295-349) · airframe 37,287 hrs · 26,838 cycles

CORROSION FOUND ON INTERCOSTALS FROM FS 295 TO FS 349 ON STRINGER # STGR 19RH BELOW WL 72.00 UNDER THE SERVICE DOOR AREA (C-CHECK RO 4/20/2021) AFTER FURTHER INVESTIGATION DAMAGE FOUND TO BE ON STR20R NOT STR19R. REMOVED AND REPLACED CORRODED INTERCOSTAL AT STR20R FROM FS310 TO FS349 AND ATTACHING GUSSET, DOUBLER AND 3EA CLEATS IAW CRJ700 SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-06 AND 51-25-16.

Part: DOUBLER — CHAFED (ZONE 200) · airframe 35,674 hrs · 25,476 cycles

PREVIOUS REPAIR AT F.S. 977.00 STRINGER 27 IS CHAFED. C/A:REO 670-53-00-528 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR PER EXPRESS JET GMM 3-3 PROCEDURES, PRIOR TO THE AIRCRAFT BEING RETURNED TO SERVICE.

Part: HINGE — GOUGED · airframe 35,674 hrs · 25,476 cycles

PASSENGER DOOR HINGE DOOR SIDE LUGS 2,5,6, AND 12 FROM FRONT ARE GOUGED. REPAIRED THE DOOR HINGE LUGS IAW REO 670-52-11-511, 670-52-11-995, EC/TC REO670-52-11-511, AND 670-52-11-995.

Part: FLOOR SUPPORT — CORRODED (BS 533-581) · airframe 35,674 hrs · 25,476 cycles

LEFT FLOOR SUPPORT BETWEEN BS 533 TO 581 IS CORRODED. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-21-1483, AND REO 670-53-21-1483.

Part: FRAME — CORRODED (BS 364) · airframe 35,674 hrs · 25,476 cycles

BS 364 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 26R. REMOVED AND REPLACED THE FRAME IAW REO 670-53-21-687, REV, 670-53-21-1481, REV --, REO 670-53-21-687, AND REO 670-53-21-1481.

Part: FRAME — CORRODED (BS 280) · airframe 35,674 hrs · 25,476 cycles

BS 280 FRAME WAS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-1478 AND REO 670-53-21-1478.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,674 hrs · 25,476 cycles

LEFT INTERCOSTAL AT STRINGER 26L IS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,674 hrs · 25,476 cycles

INTERCOSTAL AT STRINGER 27L WAS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,674 hrs · 25,476 cycles

INTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN BS 349, AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333-349) · airframe 35,674 hrs · 25,476 cycles

STRINGER SPLICE 25R IS CORRODED BETWEEN BS 333 AND 349. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 35,674 hrs · 25,476 cycles

FRAME BS 310 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EO 670-53-21-799 01, REV D.

Part: FRAME — CORRODED (BS 333) · airframe 35,674 hrs · 25,476 cycles

FRAME BS333 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-799 03.

Part: FRAME — CORRODED (BS 319) · airframe 35,674 hrs · 25,476 cycles

FRAME BS 319.7 IS CORRODED BETWEEN STRINGERS 27 AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799 02.

Part: FRAME — CORRODED (BS 295) · airframe 35,674 hrs · 25,476 cycles

FRAME BS 295 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799.

Part: BUTTSTRAP — CORRODED (BS 333) · airframe 35,674 hrs · 25,476 cycles

CIRCUMFERENTIAL BUTTSTRAP IS CORRODED AT BS 333 BETWEEN STRINGERS 25L AND 25R. REPAIRED THE CIRCUMFERENTIAL BUTTSTRAP IAW REO 670-53-21-1479, AND EC/TC REO670-53-21-1479.

Part: STRINGER — CORRODED (BS 333-364) · airframe 35,674 hrs · 25,476 cycles

STRINGER 25R CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER 25R IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 295-310) · corrosion level 2 · airframe 35,674 hrs · 25,476 cycles

STRINGER 25R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 333-364) · airframe 35,674 hrs · 25,476 cycles

STRINGER 26R IS CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 295-310) · corrosion level 2 · airframe 35,674 hrs · 25,476 cycles

STRINGER 26R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 280-333) · airframe 35,674 hrs · 25,476 cycles

STRINGER 25L IS CORRODED BETWEEN BS 280 AND 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,674 hrs · 25,476 cycles

RT INTERCOSTAL AT STRINGER 26R IS CORRODED BETWEEN FS 349.00 AND FS 364.00. REMOVED AND REPLACED INTERCOSTAL P/N SH670-32077-4 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: DOUBLER — CRACKED (FLOOR PANEL) · airframe 35,674 hrs · 25,476 cycles

RT FORWARD EQUIPMENT COMPARTMENT FLOOR PREVIOUS REPAIR IS CRACKED AT BS 193. REMOVED AND REPLACED THE REPAIR DOUBLER IAW REOS 670-53-11-509, 670-53-11-1355, AND EC/TC REO 670-53-11-1355.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,674 hrs · 25,476 cycles

STRINGER 27 FWD SEGMENT FS 310.00-333.00, AFT SEGMENT FS. 333.00-349.00 AND STRINGER SPLICE AT FS 333.00 ARE CORRODED. REMOVED AND REPLACED STRINGER 27 FWD SEGMENT PN SH670-31635-3, JOINT PN SH670-32429-3, AND AFT SEGMENT PN SH670-31371-3S IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: DOOR FRAME — CRACKED (E/E BAY DOOR) · airframe 35,674 hrs · 25,476 cycles

LEFT FORWARD EQUIPMENT BAY DOOR LANDING IS CRACKED NEAR AFT DOOR LATCH. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-06-001-001-A01 REO 670-53-11-1356, AND EC/TC REO 670-53-11-1356.

Part: DOOR FRAME — CRACKED (E/E BAY DOOR) · airframe 35,674 hrs · 25,476 cycles

RIGHT FORWARD EQUIPMENT COMPARTMENT DOOR LANDING IS CRACKED IN TWO LOCATIONS NEAR FWD AND AFT DOOR LATCHES. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-06-001-001-A01, REO 670-53-11-1356, AND EC/TC REO 670-53-11-1356.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 35,674 hrs · 25,476 cycles

BS 280 J ANGLE IS CORRODED ON UPPER FLANGE BETWEEN LBL 11 AND RBL 11. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.

Part: BRACKET — CORRODED (BS 319-349) · corrosion level 2 · airframe 35,674 hrs · 25,476 cycles

WEB PROTECTOR BRACKETS ON GALLEY SERVICE DOOR FLOOR SUPPORT ARE CORRODED. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 35,674 hrs · 25,476 cycles

RIGHT SIDE FLOOR SUPPORT IS CORRODED BETWEEN BS 280 BULKHEAD TO BS 319. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01, SH670-32170-S01, AND SH670-32170-S01.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 35,674 hrs · 25,476 cycles

RIGHT INBOARD FLAP NR 1 ACTUATOR HAS TWO FRAYED BONDING WIRES AND THE FLAP INNER SKIN IS CHAFED. COMPLIED WITH REO 670-57-52-352, AND REO 670-57-52-352, REV --.

Part: FLOOR SUPPORT — GOUGED (CARGO BAY) · airframe 35,674 hrs · 25,476 cycles

FWD CARGO BAY FLOORBOARD LANDING IS GOUGED IN TWO LOCATIONS, INBOARD OF FWD CARGO DOOR. REO 670-53-31-427 HAS BEEN ACCOMPLISHED. RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 34,398 hrs · 24,545 cycles

RECEIVED A SMOKE AFT LAV ALERT DURING DESCENT, NO SMOKE OBSERVED. MX PERFORMED AN OPS CHECK OF THE AFT LAVATORY SMOKE DETECTOR, NO FAULTS FOUND. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,325 hrs · 24,488 cycles

FWD SIDE OF BULKHEAD AT FS 202.75 FOUND INDICATION ON TOP OF STIFFENER RBL 30 APPROXIMATELY 1/4" L, STIFFENER FAILED NDT INSPECTION. REPAIRED RBL 30 POST AT FS 202.75 IAW SRM 53-11-10-201-005-A01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,325 hrs · 24,488 cycles

FWD SIDE OF BULKHEAD AT FS 202.75 FOUND INDICATION ON TOP OF STIFFENER LBL 30 APPROXIMATELY 1/4" L, STIFFENER FAILED NDT INSPECTION. REPAIRED LBL 30 POST AT FS 202.75 IAW SRM 53-11-10-201-005-A01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,325 hrs · 24,486 cycles

WHILE PERFORMING SB670BA-53-040, FOUND STR 3 TO BE CRACKED. REPAIRED STR 3 IAW REO 670-53-21-493.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,569 hrs · 23,931 cycles

FLOORBEAM AT LBL9 CORRODED BEYOND LIMITS. PERFORMED BEAM SPLICE REPAIR IAW EC/TC EO 700-53-0373.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,569 hrs · 23,931 cycles

FLOORBEAM AT RBL9 CORRODED BEYOND LIMITS. PERFORMED BEAM SPLICE REPAIR IAW EC/TC EO 700-53-0377 AND REO 670-53-61-1303.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,569 hrs · 23,931 cycles

FLOORBEAM AT LBL27 CORRODED BEYOND LIMITS. PERFORMED BEAM SPLICE REPAIR IAW EC/TC EO 700-53-0375 AND SRM 53-00-41-201-001-A01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,500 hrs · 23,077 cycles

EMERGENCY LIGHT INOPERATIVE AT CEILING PANEL ROW 7. RELAMEPD BULB IN EMERGENCY FLOOD LIGHT ABOVE ROW 7 IAW AMM 33-51-09. OPS CHECK GOOD.

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 31,843 hrs · 22,568 cycles

PASSENGER DOOR DIFFICULT TO OPEN. PASSENGER DOOR POWER ASSIST SYS: POWER ASSIST SUB-SYSTEM, MOTOR, CONTROL SWITCH, CABLES, PULLEYS, FITTINGS. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08, IPC REF; 52-11-08, ITEM 25, FIG 01, R & R POWER DOOR ASSIST SWITCH IAW AMM 20-41-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,218 hrs · 22,103 cycles

ISLE 6 CEILING EMEGENCY LIGHT INOPERATIVE. R & R ISLE 6 CEILING EMERGENCY LIGHT IAW AMM 33-21-01. OPS CHECK GOOD.

Part: LAMP — ODOR (CABIN LIGHTS) · airframe 30,930 hrs · 21,862 cycles

ELECTRICAL ODOR IN FLIGHT. F/A REPORTS SIDEWALL LIGHTS ASSOCIATED WITH ODOR, SOMEWHERE AROUND ROW 13B, CABIN INTERIOR LIGHTS: ACFT WITH FLUORESCENT LIGHTS. RELAMPED SIDEWALL LIGHTS AT 12AB IAW AMM 33-21-07. OPS CHECK GOOD. NO BURNING ODOR. DMIL CLEARED PLACARD REMOVED.

Part: SKIN — CRACKED (RT WING) · airframe 29,823 hrs · 20,955 cycles

RT WING LOWER PLANK HOLE HAS CRACK INDICATION, MARKED. RECEIVED AND COMPLIED WITH REO 670-57-21-770 P1 AND P2 AS REQUIRED. RECEIVED AND COMPLIED WITH FINAL DISPOSITION EC/TC REO 670-57-21-770.

Part: SEAT TRACK — CORRODED (BS 572-677) · airframe 29,823 hrs · 20,955 cycles

LT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 572 TO FS 677. REMOVED CORROSION AS REQUIRED AND EVALUATED DAMAGE AREA IAW SRM 53-31-49-101-001-A01 AND REO 670-53-00-013. REMOVED CORROSION AND AFTHER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-A01 AND IAW REO 670-53-00-013. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED LT SIDE SEAT RAIL FROM FS 572 TO FS 677 IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE SIDE SEAT RAIL, LT AT FS 572-677 IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-714) · airframe 29,823 hrs · 20,955 cycles

RIGHT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 677 TO FS 714. FOUND RT SIDE SEAT RAIL TO BE OUT OF LIMITS FROM FS 677-FS 714 REF GREO 670-53-00-013. REMOVED AND INSTALLED NEW FABRICATED RT SIDE SEAT RAIL FROM FS 677 TO FS 714 IAW AMM 53-00-49-000-801-A03 53-00-49-400-801-A03. FABRICATED NEW SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343, GREO 670-53-00-343, REV J AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 29,823 hrs · 20,955 cycles

RT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 485 TO FS 572. FOUND RT SIDE SEAT RAIL TO BE OUT OF LIMITS FS 485 TO FS 572 REF SRM 53-31-49-101-001-A01. REMOVED AND INSTALLED NEW FABRICATED SEAT SIDE RAIL IAW AMM 53-00-49-400-801-A03 AND AMM 53-00-49-000-801-A03. FABRICATED NEW SEAT RAIL IAW EC/TC 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 29,823 hrs · 20,955 cycles

LEFT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 863 TO FS 969. REMOVED CORROSION AND AFTER FURTHER EVALUATION FOUND TO BE BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01 AND IAW REO 670-53-00-013. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-51-00-343, REV J AS WRITTEN. REMOVED LT SIDE SEAT RAIL FS863 TO FS969 IAW SMM 53-00-49-000-801-A03. INSTALLED NEW FABRICATED LT SIDE SEAT RAIL FROM FS863 TO FS969 IAW AMM 53-00-49-400-801 A03.

Part: SEAT TRACK — CORRODED (BS 469-581) · airframe 29,816 hrs · 20,948 cycles

LBL9 SEAT RAIL HAS CORROSION. SEAT RAIL SECTION FS 469-581. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A03. INSTALLED NEW FABRICATED SEAT RAIL AT LBL 9, FS 469-FS 581 IAW AMM 53-00-49-400-81-A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 572-677) · airframe 29,823 hrs · 20,955 cycles

RIGHT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 572 TO FS 677. FOUND RT SIDE SEAT RAIL TO BE OUT OF LIMITS FROM FS 572-FS 677 REF GREO 670-53-00-613. REMOVED RT SIDE SEAT RAIL FROM FS 572 TO FS 677 IAW AMM 53-00-49-000-801-A03. INSTALLED NEW FABRICATED RT SIDE SEAT RAIL IAW AMM 53-00-49-400-801-A03. FABRICATED NEW SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 863-696) · airframe 29,823 hrs · 20,955 cycles

RT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 863 TO FS 969 AND GOUGED IN 1 LOCATION. FOUND RT SEAT RAIL TO BE OUT OF LIMITS BETWEEN FS 863-FS 969 REF GREO 670-53-00-013. R & R RT SIDE SEAT RAIL FROM FS 863 TO FS 969 IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03. FABRICATED NEW SEAT RAIL IAW EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. SDR CLOSED.

Part: SEAT TRACK — CORRODED (BS 581-680) · airframe 29,823 hrs · 20,955 cycles

LBL9 SEAT RAIL HAS CORROSION. SEAT RAIL SECTION BS 581-680. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A03. INSTALLED NEW FACRICATED SEAT RAIL, LBL9, F5 581-680 IAW AMM 53-00-49-400-801-A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 714-761) · airframe 29,823 hrs · 20,955 cycles

RT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 714 TO FS 761. FOUND RT SIDE SEAT RAIL TO BE OUT OF LIMITS FROM FS 714-FS761 REF GREO 670-53-00-013. R & R RT SIDE SEAT RAIL IAW AMM 53-00-49-000-801, 53-00-49-400-801 CONFIG, A03. FABRICATED NEW SEAT RAIL IAW ECTC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,823 hrs · 20,955 cycles

RT SIDE 280 WEB IS CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594-01 GREO 670-53-11-594 REV DATED: 04/27/2011.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 29,823 hrs · 20,955 cycles

LEFT SIDE SEAT RAIL CORRODED IN MULTIPLE PLACES FROM BS 485 - 572. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-31-419-101-001-S01. COMPLIED WITH ECTC REO 670-53-00-343 AND REO 670-51-00-343, REV J AS WRITTEN. REMOVED LT SIDE SEAT RAIL FS485-572 IAW AMM 53-00-49-000-801-A03. REPLACED LT SIDE SEAT RAIL FS485-572 IAW AMM 52-00-49-400-801-A03 AND ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,823 hrs · 20,955 cycles

LEFT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 785 TO FS 863. REMOVED CORROSION AND AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01 AND IAW REO 670-53-00-013. COMPLIED WITH ECTC REO 670-53-00-343, GREO 670-53-00343 REV J AS WRITTEN. REMOVED LT SIDE SEAT RAIL AT FS 785-FS 863 IAW AMM 53-00-49-000-801-A03. REPLACED LT SIDE SEAT RAIL AT FS 785-863 IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 714-761) · airframe 29,823 hrs · 20,955 cycles

LEFT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 714 TO FS 701. REMOVED CORROSION AND AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01 AND REO 670-53-00-013. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED LEFT SIDE SEAT RAIL FS 714 TO FS 761 IAW AMM 53-00-49-000-801, A03. INSTALLED NEW LT SIDE SEAT RAIL FROM FS 714-761 IAW AMM 53-00-49-400-801 A03.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,823 hrs · 20,955 cycles

LT SIDE 280 WEB IS CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV-DATED: 04/27/2011.

Part: SEAT TRACK — CORRODED (BS 677-714) · airframe 29,823 hrs · 20,955 cycles

LEFT SIDE SEAT RAIL CORRODED IN MULTIPLE LOCATIONS FROM FS 677 TO FS 714. REMOVED CORROSION AND AFTER FURTHER EVALUATION FOUND TO BE BE OUT OF LIMITS IAW SRM 53-31-419-101-001-S01 IAW REO 670-53-00-13. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-51-00-343 REV J AS WRITTEN. REMOVED LT SIDE SEAT RAIL FS677 TO FS714 IAW SMM 53-00-49-000-801-A03. INSTALLED NEW FABRICATED LT SIDE SEAT RAIL FROM FS 677 TO FS 714 IAW AMM 53-00-49-400-801 A03.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 29,816 hrs · 20,948 cycles

LT FLOOR SUPPORT AT BS 319 IS CORRODED. R & R LT FLOOR SUPPORT IAW DR SH670-31825, SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 29,816 hrs · 20,948 cycles

FLOOR SUPPORT AT FS 319, LBL2 IS CORRODED. REMOVED CORROSION ON FLOOR SUPPORT BRACKET FS319, CBL2 IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REPLACED FITTING IAW SRM 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 29,816 hrs · 20,948 cycles

THERE IS CORROSION ON FRAME BS 310 AT STR 26R. BLENDED CORROSION REF SRM 51-42-06-001-001 & SRM 51-21-06-001-001-A01. REPAIRED IAW STS EA 32-2015-108 AND DWG SH670-31630. RECEIVED EO 32-2015-108 AND COMPLIED WITH EA 32-2015-108.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,816 hrs · 20,948 cycles

FLOORBEAM AT THE 280 FRAME IS CORRODED. R & R FLOORBEAM IAW DWG LC 670-34256, SRM 51-42-06-001-001-A01.

Part: MEGAPHONE — INTERMITTENT (CABIN) · airframe 28,054 hrs · 19,600 cycles

F/A REPORTS MEGAPHONE INTERMITTENT. R & R MEGAPHONE IAW AMM 25-61-14.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 26,772 hrs · 18,698 cycles

EXIT SIGN ON SERVICE DOOR MISSING. REPLACED MISSING EXIT SIGN COVER IAW AMM 33-51-11.

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 26,445 hrs · 18,467 cycles

CABIN MEGAPHONES IS STUCK ON. REPLACED MEGAPHONE IAW AMM 25-61-14.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,755 hrs · 17,948 cycles

NR 5 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 25,526 hrs · 17,770 cycles

SERVICE DOOR LOWER SEAL STRIKER CORRODED. REWORKED IAW SRM 51-21-16-001-001-A01 AND SRM 51-25-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,526 hrs · 17,770 cycles

FOUND SERVICE DOOR ANGLE LOWER SILL CORRODED. REMOVED ANGLE LOWER SILL FROM SERVICE DOOR, INSTALLED SERVICEABLE ANGLE LOWER SILL, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,575 hrs · 17,807 cycles

FOUND SERVICE DOOR ANGLE LOWER SILL CORRODED. REMOVED ANGLE LOWER SILL FROM SERVICE DOOR OBTAINED NEW SERVICEABLE ANGLE DRILL DEBURR HOLES AND TRANSFER BONDING BRACKETS IAW SRM 51-40-11-01-001, 51-42-06-001-001-A01, 51-22-00-001-001. INSTALLED SERVICEABLE ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: SKIN — BURNED (BS 265) · airframe 25,526 hrs · 17,770 cycles

ONE BURN ON RIVET AND SKIN AT FS 265 ONE INCH BELOW STRINGER 20R. REPAIRED IAW REO 670-53-00-388. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,526 hrs · 17,770 cycles

LATCH PIN INTERCOSTALS BETWEEN STR 26LT AND 26R CORRODED FROM FS 349-364. REMOVED TWO CORRODED INTERCOSTALS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED TWO NEW SERVICEABLE INTERCOSTALS BETWEEN STGR 26L AND 26R FS 349.0 - 364.0 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-32050, SH670-32075. REPAIR IS CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (BS 310-349) · airframe 25,526 hrs · 17,770 cycles

ASD THRESHOLD CORRODED IN MULTIPLE LOCATION OF SILL PLATE BETWEEN FS 310-349. REPAIRED IAW SRM 51-42-06-001-001 & 51-42-21-001-001.

Part: SKIN — BURNED (BS 437) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET ON FS 437 BETWEEN S16 - 17R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 517 S6R) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET ON STRINGER 6R, FOUR INCHES AFT OF FS 517. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 581) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET 6.5 INCHES AFT OF FS 581 ON S15R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 364) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET AND SKIN AT TWO INCHES AFT OF FS 364.00 ON S8R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 310) · airframe 25,503 hrs · 17,755 cycles

BURNED SKIN AT 4" FWD OF FS 310.00 AND STR17 RT. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 202) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON SKIN FIVE INCHES AFT OF FS 202 BETWEEN S19 - 20R. REPAIRED IAW 670-53-00-388.

Part: SKIN — BURNED (BS 597) · airframe 25,525 hrs · 17,769 cycles

ONE BURN AT FS 597 ONE INCH ABOVE S5R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 517) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET ON FS 517, BELOW STR 16R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 453) · airframe 25,503 hrs · 17,755 cycles

BURN ON SKIN EDGE FWD FS 453 BELOW STRINGER 8R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 250) · airframe 25,503 hrs · 17,755 cycles

ONE BURN ON SKIN AT FS 250 AND ONE INCH BELOW STRINGER 20R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 394) · airframe 25,503 hrs · 17,755 cycles

BURN ON SKIN FWD OF FS 394 ON STR 12R. REPAIRED IAW REO NR 670-53-00-388.

Part: SKIN — BURNED (BS 202) · airframe 25,503 hrs · 17,755 cycles

ONE BURN ON SKIN 7 INCHES AFT OF FS 202 STRINGER 18R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 409) · airframe 25,503 hrs · 17,755 cycles

BURN ON SKIN AFT OF BS 409 BELOW STR 8R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 409) · airframe 25,503 hrs · 17,755 cycles

BURN ON SKIN FWD OF FS 409 BELOW STR 8R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 613 S1R) · airframe 25,525 hrs · 17,769 cycles

ONE BURNED RIVET ON FS 613 ONE INCH BELOW S1R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 693) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET ONE INCH AFT OF FS 693 ON S10R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 549) · airframe 25,525 hrs · 17,769 cycles

ONE BURN ON RIVET SIX INCHES FWD OF FS 549 ON S16R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 437-421) · airframe 25,503 hrs · 17,755 cycles

BURN ON SKIN BETWEEN FS 437 - 421 BELOW STRINGER 8R. REPAIRED IAW REO 670-53-00-388.

Part: SKIN — BURNED (BS 280) · airframe 25,503 hrs · 17,755 cycles

ONE BURN ON SKIN AT BS 280 STRINGER 20R. REPAIRED IAW REO 670-53-00-388.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 25,503 hrs · 17,755 cycles

SERVICE DOOR THRESHOLD CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 310 -349. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 833-985) · airframe 25,503 hrs · 17,755 cycles

SEAT TRACK LBL 9 BS 833-985 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-681) · airframe 25,503 hrs · 17,755 cycles

SEAT TRACK LBL 9 FS 581-681 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 25,502 hrs · 17,754 cycles

RT SIDE SEAT TRACK CORRODED AT FS 708. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 25,502 hrs · 17,754 cycles

LT SIDE SEAT TRACK CORRODED AT FS 581. REPLACED WITH SERIVCABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-681) · airframe 25,502 hrs · 17,754 cycles

SEAT TRACK RBL 9, FS 581-681 IS CORRODED SEVERAL AREAS. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-8901-A03.

Part: SEAT TRACK — CORRODED (BS 693-833) · airframe 25,503 hrs · 17,755 cycles

SEAT TRACK LBL 9 BS 693-833 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED NEW IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 25,502 hrs · 17,754 cycles

LT SIDE SEAT TRACK CORRODED AT FS 708. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 481-570) · airframe 25,502 hrs · 17,754 cycles

LT SIDE SEAT TRACK FS 481 - 570 CORRODED AT SEVERAL AREA. REPLACED WITH A NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 570-673) · airframe 25,502 hrs · 17,754 cycles

RT SIDE SEAT TRACK FS 570-673 CORRODED IN SEVERAL AREAS. REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49-400-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785.15-860) · airframe 25,502 hrs · 17,754 cycles

RT SIDE SEAT TRACK FS 785.15-860 CORRODED IN SEVERAL AREAS. REPLACED WITH NEW SERVICABLE SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-481) · airframe 25,502 hrs · 17,754 cycles

RT SIDE SEAT TRACK FS 379-481 CORRODED IN SEVERAL AREAS. REPLACED RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 25,502 hrs · 17,754 cycles

SEAT TRACK RBL 9 CORRODED AT BS 349. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 736) · airframe 25,502 hrs · 17,754 cycles

LT SIDE SEAT TRACK CORRODED AT FS 736.05. REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-860) · airframe 25,502 hrs · 17,754 cycles

LT SIDE SEAT TRACK FS 785.15-860 CORRODED IS SEVERAL AREAS. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A01 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 833-985) · airframe 25,503 hrs · 17,755 cycles

SEAT TRACK RBL 9 BS 833-985 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED IAW 53-00-49.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

RT SIDE FLOOR SUPPORT CORRODED AT FS 280. INSTALLED NEW RT FS 280 FLOOR SUPPORT IAW SRM 51-42-06-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

LT SIDE BS 280 FLOORBEAM CORRODED. REPLACED FLOORBEAM IAW SRM 53-11-41-201-003-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

RT SIDE BS 280 FLOORBEAM CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: ANGLE — CORRODED (BS 1015-1047) · airframe 25,502 hrs · 17,754 cycles

AFT CARGO DOOR SILL ANGLE CORRODED IN SEVERAL AREAS BETWEEN FS 1015 AND 1047. REPAIRED IAW REO 670-53-61-913, REV A.

Part: BULKHEAD — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

RT SIDE BS 280, BULKHEAD WEB CORRODED. REPAIRED IAW REO 670-53-11-594.

Part: FLOOR SUPPORT — CORRODED (BS 992) · airframe 25,502 hrs · 17,754 cycles

RT CARGO FLOOR SUPPORT CORRODED AT FS 992.00. REPAIRED IAW STEPS 1, 2, AND 3 OF REO 670-53-61-959.

Part: FLOOR SUPPORT — CORRODED (BS 985) · airframe 25,502 hrs · 17,754 cycles

LT CARGO FLOOR SUPPORT CORRODED AT FS 985.00. REPAIRED IAW STEPS 1, 2, AND 3 OF REO 670-53-61-959.

Part: FLOORBEAM — CORRODED (BS 1051.3) · airframe 25,502 hrs · 17,754 cycles

AFT CARGO FLOORBEAM AT FS 1051.3 CORRODED AT RBL 38. REPAIRED IAW REO 670-53-61-957.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

LT BS 280 BULKHEAD WEB CORRODED. REPAIR IAW REO 670-53-11-594.

Part: POST — CORRODED (BS 280 BULKHEAD) · airframe 25,502 hrs · 17,754 cycles

RT SIDE BS 280 BULKHEAD VERTICAL POST CORRORED AT FLOOR LINE AFT CORNER. REPAIRED IAW STEP 1 OF REO 670-53-11-829, REF ITEM 7.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,502 hrs · 17,754 cycles

FLOORBEAM CORRODED AT FWD SIDE OF BS 280. REPLACED FLOORBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 364 S26R) · airframe 25,502 hrs · 17,754 cycles

STRINGER 26R HAS CORROSION AT FS 364. REPAIRED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 349) · airframe 25,502 hrs · 17,754 cycles

FRAME BS 349 HAS CORROSION AT STR 27. REPAIRED IAW WITH STPS 1, AND 2 OF REO 670-53-21-941.

Part: SKIN — GOUGED (BS 980) · airframe 25,502 hrs · 17,754 cycles

GOUGE IN FUSELAGE BELLY AT FS 980 CENTER BOTTOM OF ACFT. REPAIRED IAW REO 670-53-00-387.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,502 hrs · 17,754 cycles

AFT DRAG ANGLE CRACKED BY MOTOR PULLEY BRACKET. REPAIR ANGLE IAW SRM 52-11-04-201-002-A01.

Part: SKIN — BURNED (BS 173-693) · airframe 25,526 hrs · 17,770 cycles

EIGHT RIVETS BETWEEN BS 173 AND 693 S5-22 HAVE LIGHTNING STRIKE DAMAGE. COMPLIED WITH PERMANENT REPAIR IAW SRM 53-00-00-201-003-A01 AND REO ECTC 670-53-00-388. REPAIR CLASSIFIED AS MAJOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,520 hrs · 17,081 cycles

INTERIOR CEILING EMERGENCY LIGHT AT 10ABCD IS OUT. LAMPED INTERIOR CEILING EMERCENCY LIGHT AT SEATS 10ABCD IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,071 hrs · 16,763 cycles

RT PACK CAUTION, FOLLOWED BY ODOR IN THE COCKPIT SIMILAR TO SULFUR . THE FA SAID CABIN FILLED WITH SMOKE. RAN EVACUATION CHECKLIST. EMERGENCY DECLARED, CHECKED RT & LT AIR CYCLE MACHINE (ACM) IAW AMM 21-51-08. OPS CHECKED GOOD. NO DEFECT NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,077 hrs · 16,008 cycles

CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 22,759 hrs · 15,787 cycles

EMERGENCY LIGHTS IN ARMED POSITION ARE ON. PERFORMED FUNCTIONAL RESET OF ACFT IAW AMM 24-00-00. FUNCTION CHECKED OK NO FURTHER DEFECTS NOTED.

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 22,513 hrs · 15,615 cycles

LEFT WING ANTI ICE INDICATION AFTER TAKE OFF, QRH ACCOMPLISHED, WITHIN SEC WING OVERHEAT POSTED, QRH C/W AGAIN. BOTH RT AND LT WING ANTI ICE NOW POSTED AND INTERMITTENT FOR REMAINDER OF FLT APPROX 6 MIN, AND SO ON UNTIL LANDING. WING ANTI-ICE MODULATING AND SHUTOFF VALVES ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. REPLACED LEFT WING ANTI-ICE VALVE IAW AMM 30-12-02, OP'S CHECKED GOOD.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHTS) · airframe 22,035 hrs · 15,289 cycles

EMERGENCY LIGHTS BLINKING OFF AND ON IN THE ARMED POSITION. R & R PCB 5 IN JB11 IAW AMM 24-06-11-710-801. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,760 hrs · 15,098 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,522 hrs · 14,932 cycles

NR 2 CEILING BATTERY PACK INOPERATIVE. R & R NR 2 CEILING EMERGENCY LIGHTING BATTERY PACK IAW AMM 33-51-17 AND IPC 33-51-17, ITEM 6.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 20,512 hrs · 14,221 cycles

LT EMERGENCY EXIT LIGHT INOP. REPAIR WIRING. FOUND 2 WIRES PULLED OUT OF P347 FOR EXIT SIGN DS174. REQUIRED WIRES BY CRIMPING NEW CONTACTS ON WIRES IAW ESPM CH 20-16-00. REMOVED THE LT OVERWING EMERGENCY EXIT PANEL IAW AMM 25-26-09-000-801. OK TO CLOSE MAC9QC 4/14/11 INSTALLED THE LT OVERWING EMERGENCY EXIT PANEL (261ELW) IAW AMM 25-26-09-400-801. PERFORM OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TEST GOOD.

Part: FRAME — CORRODED (BS 295) · airframe 20,512 hrs · 14,221 cycles

FRAME AT FS 295 CORRODED ON AFT SIDE ON VERTICAL. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 333 S26-27L) · airframe 20,512 hrs · 14,221 cycles

FRAME AT 333 BETWEEN STRINGERS 27 AND 26L CORRODED ON BOTH SIDES, VERTICAL LEG AND ON HORIZONTAL LEG. REPAIRED IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 333 S26R) · airframe 20,512 hrs · 14,221 cycles

FRAME AT FS 333.00 AT STR 26RT IS CORRODED. REPAIRED IAW SRM 51-42-06-011-011-A01.

Part: SKIN — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

CORROSION IN BELLY JUST AFT 280.00 ON END STRAP BETWEEN STRINGERS 25R AND 25L. REPAIRED IAW REO 670-53-676.

Part: FRAME — CORRODED (BS 319) · airframe 20,512 hrs · 14,221 cycles

FWD SIDE FRAME 319.00 CORRODED ON VERTICAL AND HORZ LEGS OF STR 26L. REPAIRED AREA IAW SRM 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364 S27R) · airframe 20,512 hrs · 14,221 cycles

INTERCOSTAL JUST FWD OF FS 364.00 JUST RT OF STR 27, CORRODED ON BOTH SIDES OF VERT LEG AND ON HORIZ LEG. REMOVED INSOLATION AT FS 364.00 BETWEEN S25L & S25R IAW AMM 25-84-00-000-801-A04. INSTALLED INSULATION AT FS 364.00 BETWEEN S25L & S25R IAW AMM 25-84-00-000-801-A04. REMOVED 3 EA FASTENERS THRU SKIN AND PROX SWITCH & MOUNT BRACKET. BLENDED DAMAGED AREA REF SRM 51-42-06-001-001. FOUND INTERCOSTAL TO BE OUT OF LIMITS. SRM 53-21-23-101-003 STEP 3B(5). REMOVED DAMAGED INTERCOSTAL AND DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. THIS IS A MINOR REPAIR. INSTALLED INTERCOSTAL AT FWD OF FS 364 NEXT TO STR 27, ALL WORK DONE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001. TOP COATED HEAD OF RIVETS AND WORK DONE IAW SRM 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-358) · airframe 20,512 hrs · 14,221 cycles

CABIN SEAT TRACK CORRODED BETWEEN FS 349.00-358.00, RBL 9.0. FOUND TO BE OUT OF LIMITS 53-21-49. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

CORROSION ON FS 280 CROSSBEAM. REMOVED SURFACE CORROSION IAW SRM 51-21-03-001-001-A01. TREATED AREA, PRIMED, AND PAINTED IAW SRM 51-21-06-001-001-A01. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 453) · airframe 20,512 hrs · 14,221 cycles

CABIN SEAT TRACK GOUGED AT FS 453.00, RBL 9.0. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01 AND SRM 53-21-49-101-001-A01. FOUND SEAT RAIL TO BE OUT OF LIMITS IAW 53-21-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: WEB — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

RT FS 280.00 LOWER WEB CORRODED. REMOVED WEB IAW 51-42-06-001-001-A01 AND INSTALLATION OF NEW WEB IAW SRM 53-11-10, REPAIR "B".

Part: FLOOR SUPPORT — CORRODED (E/E BAY) · airframe 20,512 hrs · 14,221 cycles

FLOOR SUPPORT BRACKET FOR AVIONICS FLOORBOARD 141ALF AT FS 280.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. TREATED AREA, PRIMED AND PAINTED IAW SRM 51-21-06-001-001-A01. MINOR REPAIR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 20,512 hrs · 14,221 cycles

2 EA CLIPS CORRODED ON LOWER PAX DOOR (INBD AND OTBD, FS 340) (OPEN).

Part: SEAT TRACK — CORRODED (BS 549-581) · airframe 20,512 hrs · 14,221 cycles

9R FLOOR SEAT TRACK CORRODED BETWEEN FS 549 AND 581. FOUND SEAT RAIL TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801. BLENDED CORROSION IAW SRM 53-31-49-101-001-A01 AND SRM 51-21-06-001-001-A01. INSTALLED NEW SEAT RAIL FS 485 TO FS 581 IAW AMM 53-00-49-400-801. THIS IS A MINOR REPAIR.

Part: CHANNEL — CORRODED (BS 318) · airframe 20,512 hrs · 14,221 cycles

LOWER CHANNEL HAS CORROSION INBD SIDE JUST AFT OF FWD CORNER APPROX FS 318. REMOVED CORROSION IAW SRM 51-12-06-001-001-A01. BLEND AREA FOUND TO BE WITHIN LIMITS IAW SRM 52-11-01-101-001. MINOR REPAIR.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

CORROSION ON FS 280 CROSSBEAM.

Part: FRAME — CORRODED (BS 310 S26L/R) · airframe 20,512 hrs · 14,221 cycles

FRAME AT FS 310, STR 26L TO 26R CORRODED. REMOVED SURFACE CORROSION IAW SRM 51-21-03-001-001-A01. TREATED AREA, PRIMED, AND PAINTED IAW SRM 51-21-06-001-001-A01. MINOR REPAIR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 20,512 hrs · 14,221 cycles

TWO CLIPS CORRODED ON LOWER PAX DOOR, INBD AND OTBD OF FS 318. R & R CLIPS IAW SRM 51-42-06-001-001 AND 51-42-20-001-001. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 394-517) · airframe 20,512 hrs · 14,221 cycles

9L INBD OF SEAT TRACK CORRODED BETWEEN FS 394 AND FS 517. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 549-581) · airframe 20,512 hrs · 14,221 cycles

9L FLOOR SEAT TRACK CORRODED BETWEEN FS 549 AND 581. AFTER FURTHER EVALUATION 9L FLOOR SEAT TRACK FOUND TO BE OUT OF LIMITS. IAW SRM 51-21-03-001-001-A01 AND 53-31-49-101-001-A01. REMOVED 9L FLOOR SEAT TRACK BETWEEN FS 485.0 AND 581.0, FS IAW AMM 53-00-49-000-801. SEAT TRACK 9L BETWEEN FS 485 TO FS 581 REQUIRES INSTALLATION. INSTALLED NEW SEAT RAIL 9L FS 485 TO FS 581 IAW AMM 53-00-49-400-801. (CLOSED)

Part: FRAME — CORRODED (BS 333 S26R) · airframe 20,512 hrs · 14,221 cycles

FRAME AT FS 333.00 AT STR 26 RT IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-01-01. FOUND OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. PERFORMED UT THICKNESS INSP OF BLEND AREA IAW MAC NDT UT-3. COMPLIED WITH STEP 2 OF REO 670-53-21-677, NO INDICATIONS NOTED AT THIS TIME.

Part: WEB — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

LT FS 280.00 LOWER WEB CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 333) · airframe 20,512 hrs · 14,221 cycles

FRAME AT 333 BETWEEN STRINGERS 27 AND 26L CORRODED ON BOTH SIDES VERTICAL LEG AND ON HORIZ LEG.

Part: FRAME — CORRODED (BS 333) · airframe 20,512 hrs · 14,221 cycles

FRAME AT 333 BETWEEN STR 27 AND 26L CORRODED ON BOTH SIDES VERTICAL LEG AND ON HORIZONTAL LEG. FOUND OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. REMOVED CORROSION IAW SRM 51-21-06-01-01.

Part: FRAME — CORRODED (BS 295) · airframe 20,512 hrs · 14,221 cycles

FRAME AT 295 CORRODED ON AFT SIDE ON VERT AND HORIZ LEGS AT STR 27. OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: STRAP — CORRODED (BS 280) · airframe 20,512 hrs · 14,221 cycles

CORROSION, JUST AFT 280.00 ON END STRAP BETWEEN STR 25R AND 25L. BLENDED DAMAGE AREA IAW SRM 51-42-06-001-001 AND SRM 51-21-06-001-001.

Part: FRAME — CORRODED (BS 319 S26R) · airframe 20,512 hrs · 14,221 cycles

FWD SIDE FRAME 319.00 CORRODED ON VERTICAL AND HORIZ LEGS ON STR 26R. OUT OF LIMITS IAW 53-21-06-101-002-A01. CORROSION PENETRATED 100 PERCENT OF THICKNESS REMOVED AND REPLACED FRAME IAW REO 670-53-21-671.

Part: STRINGER SPLICE — CORRODED (BS 349 S26R) · airframe 20,512 hrs · 14,221 cycles

STRINGER SPLICE CORRODED AT 26R JUST FWD OF FS 349.00. DAMAGE BLENDED OUT OF LIMITS SRM 51-21-06-001-001. REMOVED SPLICE. INSTALLED NEW SPLICE IAW SRM 51-42-06-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,512 hrs · 14,221 cycles

ASD AFT DRAG ANGLE CRACKED. R & R DRAG ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 20,512 hrs · 14,221 cycles

WL 79.50 SKIN CRACKED AT FS 193.00 ON LT SIDE. REPAIRED IAW REO 670-53-11-509.

Part: SKIN — CRACKED (BS 193) · airframe 20,512 hrs · 14,221 cycles

WL 79.50, SKIN CRACKED AT FS 193.00 ON RT SIDE. REPAIRED IAW REO670-53-11-509.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,884 hrs · 13,795 cycles

SEVERAL MID CABIN LOWER EMERGENCY LIGHT BULBS INOP. ON LT AND RT SIDE. RELAMPED MID CABIN LOWER EMERENCY LIGHTS ON LT AND RT SIDES IAW AMM 33-51-11, OP'S CHECK GOOD. RELAMPED MID CABIN LOWER EMERENCY LIGHTS ON LT AND RT SIDES IAW AMM 33-51-11, OP'S CHECK GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,769 hrs · 13,715 cycles

NR 5 CABIN CEILING EMERGENCY LIGHT INOP,RESOLVED ON W/O: 181940 TASKCARD: N/R-00004. RELAMPED NR 5 CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. RELAMPED NR 5 CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD.

Part: BATTERY — DAMAGED (MEGAPHONE) · airframe 19,376 hrs · 13,446 cycles

MEGAPHONE WAS DAMAGED AND INOP. REPLACED DAMAGED SCREWS AND BATTERY ON MEGAPHONE IAW CMM 25-61-14. (CLOSED)

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 18,317 hrs · 12,661 cycles

GALLEY NR 2 FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER BROKE. R & R GALLEY NR 2 FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER IAW AMM 33-51-11.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,803 hrs · 12,271 cycles

CAPTAINS FLASHLIGHT INOP. R & R CAPTAIN'S FLASHLIGHT IAW AMM 25-61-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,267 hrs · 11,859 cycles

CEILING EMERGENCY LIGHT 4TH FROM FRONT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,224 hrs · 11,829 cycles

F/A FLASHLIGHT NOT WORKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,274 hrs · 11,103 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR ENTRANCE RT SIDE INOP. FLT 5593 DEL 31 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,109 hrs · 10,980 cycles

EMERGENCY LIGHTS AT RT EMERGENCY DOOR LWR AND RT GALLEY LWR BOTH HAVE A COUPLE OF BULBS BURNED OUT.

Part: HANDLE — CRACKED (DOOR) · airframe 15,764 hrs · 10,705 cycles

ASD HANDLE IS CRACKED. INSTALLED TEMP REPAIRED PER EC/TC 670-52-11-196.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

RT PAX FLOOR SEAT RAIL FS 581.00 TO FS 683.50 IS CORRODED (13259/PG 81).

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 15,656 hrs · 10,625 cycles

LT PAX FLOOR SEAT RAIL FS 683.50 TO FS 836.50 IS CORRODED (13259/PG.83).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

RT PAX FLOOR SEAT RAIL FS 683.50 TO FS 836.50 IS CORRODED (13259/PG 82).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

RT PAX FLOOR SEAT RAIL FS 350.00 TO FS 485.00 IS CORRODED. BLENDED FLOOR SEAT RAIL, MATERIAL LOSS OF .050 NOTED, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, INSTALLED SPLICE SECTION OF SEAT RAIL IAW AMM 53-00-49. INSTALLED SERVICEABLE SEAT TRACK IAW ASA AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

RT PAX FLOOR SEAT RAIL FS 485.00 TO FS 581.00 IS CORRODED (13259/PG 81).

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,656 hrs · 10,625 cycles

LT PAX FLOOR SEAT RAIL FS 485.00 TO FS 581.00 IS CORRODED. BLENDED CENTER PAX DOOR FLOOR SEAT RAIL FS 485-581 IAW SRM 51-21-11, ALL BLENDED AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-31-49, TREATED BLENDED AREAS IAW SRM 51-21-11.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 15,656 hrs · 10,625 cycles

LT PAX FLOOR SEAT RAIL FS 581.00 TO FS 683.50 IS CORRODED (13259/PG 83).

Part: SEAT TRACK — CORRODED (BS 836-988) · airframe 15,656 hrs · 10,625 cycles

RT PAX FLOOR SEAT RAIL FS 836.50 TO FS 988.00 IS CORRODED (13259/ PG 82). BLENDED CORROSION ON RT PAX FLOOR SEAT RAIL IAW SRM 51-21-11, ALL AREAS BLENDED FOUND TO BE WITHIN LIMITS IAW SRM 53-51-49, TREATED, & PRIMED BLENDED AREAS IAW SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

LT PAX FLOOR SEAT RAIL FS 374.00 TO FS 485.00 IS CORRODED (13259/PG 82).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

LEFT PAX SIDE SEAT RAIL FS 784.00 TO FS 861.00 IS CORRODED (13259/PG 84).

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 15,656 hrs · 10,625 cycles

RT PAX SIDE SEAT RAIL FS 784.00 TO FS 861.00 IS CORRODED (13259/PG 84). BLENDED CORROSION IAW SRM 53-41-49, ALL AREAS BLENDED FOUND TO BE WITHIN LIMITS IAW SRM 53-41-49. TREATED REWORKED AREAS OF RT PAX SIDE SEAT RAIL IAW SRM 51-21-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

FS 280 WEB AT LBL 9 IS CORRODED. FOUND CORROSION TO BE MINOR. BLENDED AREA REMOVING SURFACE CORROSION.

Part: BEAM — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

FS 280 BEAM AT RBL 9 IS CORRODED (13221 PG 63). CUT AWAY CORRODED AREA ON FS 280 BEAM UPPER FLANGE. FABRICATED FILLER IAW REO 670-53-11-404. INSTALLED SERVICEABLE FILLER IAW REO670-53-11-404.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,656 hrs · 10,625 cycles

SEQ 29 \ 1000-0013 FS 280 CORRODED ON RT SIDE THRESHOLD WEB ANGLE, TOP (13330 PG 56).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,584 hrs · 10,570 cycles

NR 4 CEILING EMERGENCY LIGHT INOP.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 15,280 hrs · 10,342 cycles

MEGAPHONE BATTERY DEAD.

Part: PLACARD — UNKNOWN (PAX DOOR) · airframe 14,730 hrs · 9,942 cycles

F/A ADVISES THE OPEN EXIT STICKERS ON MAIN CABIN DOOR NEED REPLACING.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 13,002 hrs · 8,670 cycles

FIRE SYS FAULT STATUS MSG CAME ON IN FLIGHT THEN EXTINGUISHED. DISCREPANCY NO LONGER EXIST.

Part: HANDLE — BINDING (PAX DOOR) · airframe 12,995 hrs · 8,664 cycles

PAX DOOR HANDLE VERY DIFFICULT TO OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 11,458 hrs · 7,630 cycles

MAIN CABIN DOOR IS HARD TO CLOSE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,359 hrs · 7,571 cycles

F/A FLASHLIGHT FWD WILL NOT STAY ON.

Part: FRAME — CORRODED (BS 310) · airframe 11,267 hrs · 7,504 cycles

CORROSION DAMAGE FS 310.00 FRAME BETWEEN STR 27 AND 26 RT IN MAIN AVIONICS BAY (MARKED). FOUND BLENDED AREA WITHIN LIMITS IAW CRJ 700 SRM 53-21-00 ONLY .002 MATERIAL REMOVED ALLOWED UP TO .005. ALODINES PRIMED AND PAINTED BLENDED AREA. INSTALLED FOUR REMOVED RIVETS IN WORKED AREA IAW CRJ 700 SRM 51-42-06.

Part: SILL — CORRODED (BS 280) · airframe 11,267 hrs · 7,504 cycles

RT FLOOR SILL AT RBL 45 FS 280 IS CORRODED OUT OF LIMITS. REPAIRED RT FLOOR SILL AT RBL 45 FS280 IAW REO 670-53-21-139

Part: DRAG ANGLE — CRACKED (TAILCONE) · airframe 11,267 hrs · 7,504 cycles

RHS VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED RS VERT STAB DRAG ANGLE PER REO 670-55-31-018

Part: DRAG ANGLE — CRACKED (TAILCONE) · airframe 11,267 hrs · 7,504 cycles

LT VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED LT VERT STAB DRAG ANGLE IAW REO 670-55-31-018

Part: ANGLE — CORRODED (BS 280) · airframe 11,267 hrs · 7,504 cycles

COCKPIT FWD 280 ANGLE (LAND) CORRODED.

Part: PLACARD — WORN (AIRSTAIR) · airframe 11,267 hrs · 7,504 cycles

ASD EXIT PLACARD WORN.

Part: ATTACH BRACKET — CRACKED (AIRSTAIR DOOR) · airframe 11,267 hrs · 7,504 cycles

ASD INTERCOSTAL ATTACH BRACKET AT LOWER FWD CORNER HAS POSSIBLE CRACK.

Part: SKIN — CRACKED (AIRSTAIR DOOR) · airframe 11,267 hrs · 7,504 cycles

ASD INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP. [07-26-07] REPLACED UPPER EDGE MEMBER PER CRJ 700 SRM 51-42-06.

Part: SKIN — CRACKED (AIRSTAIR DOOR) · airframe 11,267 hrs · 7,504 cycles

ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP.

Part: INTERCOSTAL — CRACKED (AIRSTAIR DOOR) · airframe 11,267 hrs · 7,504 cycles

ASD INTERCOSTAL AT LOWER AFT CORNER HAS POSSIBLE CRACK.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 11,249 hrs · 7,492 cycles

F/A REPORTS MEGAPHONE IS DEAD.

Part: BOLT — MISSING (PAX DOOR) · airframe 10,993 hrs · 7,297 cycles

PAX DOOR WILL NOT CLOSE AND LOCK PROPERLY, DOOR APPEARS TO BE OUT OF RIG AFT ASSY HAS CROSS OVER TUBE BOLT MISSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,418 hrs · 6,898 cycles

LEFT FUSELAGE 1 EXTERIOR EMERGENGY LIGHT INOP.

Part: WARNING MESSAGE — ACTIVATED (FIRE WARNING) · airframe 10,178 hrs · 6,743 cycles

LEFT FIRE SYSTEM FAIL CAUTION MSG. AIRCRAFT RETURNED TO ATL AFTER T/O. FLTS 4209, 4899 CX.

Part: UNKNOWN — UNKNOWN (SPOILERS) · airframe 10,011 hrs · 6,629 cycles

I/B SPOILERON AND O/B FLT SPOILER FAULT CAUTION MSG DURING APPROACH. EN ROUTE TO EYW A/C DIVERTED TO MIA AFTER T/O. EMERGENCY DECLARED.

Part: DOOR — OBSTRUCTED (PAX DOOR) · airframe 8,703 hrs · 5,804 cycles

PAX DOOR WILL NOT CLOSE STOPS ABOUT 2 INCHES. ACTS LIKE DOOR HITS SOMETHING.

Part: PLACARD — WORN (FUSELAGE) · airframe 8,282 hrs · 5,544 cycles

ASD (EXIT) PLACARD WORN.

Part: LIGHT — DETERIORATED (CABIN)

DURING C-CHECK, THE CABIN FLOOR EMERGENCY LUMINOUS LIGHT STRIPS WERE FOUND TO BE DETERIORATED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMNATION OF AN APPROPRIATE C/A. (K)

Part: HANDLE — CRACKED (FUSELAGE)

DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE MAIN AVIONICS BAY DOOR HANDLE IAW SRM. (K)

Part: PANEL — CRACKED (DOOR)

DURING A C-CHECK, THE PASSENGER DOOR AFT SIDE PANEL, AT FIRST STEP RISER, WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT SIDE PANEL, AT FIRST STEP RISER, IAW REO. (K)

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT 4911 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESET CIRCUIT BREAKER P2U3. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 4,697 hrs

DURING APPROACH, AT APPROXIMATELY 300 FT CREW RECEIVED A MASTER CAUTION SINGLE CHIME. EICAS SHOWED HYDRAULIC 2 LOW PRESSURE. PARKING BRAKE-BRAKE PRESSURE. RT THRUST REVERSER INOP, ALONG WITH FLIGHT SPOILER DEPLOY ADVISORY MESSAGES. HYDRAULIC SYNOPTIC PAGE SHOWED 35 PERCENT QUANTITY AND SYSTEM PRESSURE SHOWED ZERO WITH BOTH PUMPS OPERATING. FLIGHT CONTROL PAGE SHOWED IB FLIGHT SPOILERS TO BE SLIGHTLY DEPLOYED WITH NO DEGRADATION OF AC CONTROLLABILITY. DUE TO INSUFFICIENT FUEL CREW DECLARED AN EMERGENCY AND DIVERTED, LANDING SAFELY. MAINTENANCE PERFORMED TEMPORARY REPAIR BY REMOVING AND REPLACING THE NR 2 ELECTRIC HYDRAULIC PUMP LINE IAW REO. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: GLOWSTRIP — TORN (CABIN)

FLT 4535 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP WAS FOUND TORN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT AFT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)