N137EV

Part: BRACKET — UNKNOWN · airframe 34,499 hrs · 24,853 cycles

WHILE INCORPORATING SB 670SH-53-043 REV C, R/H VOLUMETRIC FUSE BRACKET P/N: SH698-75355-1 FOUND TO NOT WORK WITH EXISTING A/C FASTENER HOLES (LOW ED). COMPLIED WITH MHIRJ EO SH698-75355 SNIEO S10 ALL STEPS 1-5. STEP #3 IS NOT REQUIRED DUE TO THE PART BEING FABRICATED FROM PREFABRICATED MATERIAL CMS6144-14. COMPLIED WITH ALL STEPS 1-3 FOR INSTALLATION OF THE NEW BRACKET IAW MHIRJ EO KSH670-35829 NIEO S87.

Part: FITTING — NONE · airframe 34,499 hrs · 24,853 cycles

WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL 05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33562-001SB AND CC670-33563-001SB CAN NOT BE INSTALLED IAW SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING FASTENER PITCH ON THE AIRCRAFT. REPAIRED BY OMITTING A FASTENER HOLE, TRIMMING PARTS, AND INSTALLING ALTERNATE FASTENERS IAW MHIRJ REO 690-53-11-1848 REVISION - - DATED 2024-09-16.

Part: SENSOR — INOPERATIVE (BRAKE TEMP) · airframe 33,835 hrs · 24,305 cycles

BRAKE OVHT WARNING MESSAGE IN FIGHT. RAN QRH BUT MESSAGE APPEARED AGAIN. DEFERRING EICAS BRAKE TEMPERATURE MONTORING SENSOR FOR LHOB BREAK IAW MEL 32-46-1D. MMO2 UPDATED. PLACARD INSTALLED. MOC #102931 NOTIFIED. R/R LH OB BRAKE TEMP. SENSOR IAW CRJ 900 AMM 32-46-01. PERFORMED SELF-TEST OF THERMOCOUPLE IAW CRJ 900 AMM 32-46-01, OPS TEST GOOD, NO DEFECTS NOTED AT THIS TIME. MM02 UPDATED, PLACARD REMOVED, MOC NOTIFIED # 105369.

Part: BEAM — CORRODED · airframe 30,282 hrs · 21,335 cycles

FLOOR BEAM AT LBL9.00 HAS CORROSION BETWEEN FS661+24 AND 661+90. REPAIRED FLOOR BEAM PER CRJ900 SRM 53-00-43-201-001-A03 AND REO 690-53-31-651 REV -- DATED 2022-06-20

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

RH FLOOR SILL BETWEEN FS280-295 HAS AREAS OF CORROSION ON TOP AND BOTTOM SURFACES. REPLACED FLOOR SILL.

Part: ANGLE — CORRODED · airframe 30,282 hrs · 21,335 cycles

CORROSION ON LOWER SILL ANGLE (BELOW LH FWD EMER DOOR) BETWEEN FS720-744. REMOVED CORROSION AND APPLIED REPAIR ANGLE REF EA:CRJ953-13834 REV IR 6/11/2022.

Part: FRAME — CRACKED · airframe 30,282 hrs · 21,335 cycles

FRAME/SH670-36600-1/CRACKED/FRAME/SH670-36600-1 FRAME/SH670-36600-1/CRACKED

Part: FRAME — CRACKED · airframe 30,282 hrs · 21,335 cycles

LH SIDE AFT EMERGENCY EXIT DOOR HAS CRACK AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: ANGLE — CRACKED · airframe 30,282 hrs · 21,335 cycles

PAX DOOR AFT DRAG ANGLE CRACKED, REPLACED AFT DRAG ANGLE.

Part: FRAME — CRACKED · airframe 30,282 hrs · 21,335 cycles

LH SIDE FWD EMERGENCY EXIT HAS CRACKS AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: FRAME — CRACKED · airframe 30,282 hrs · 21,335 cycles

RH FWD EMERGENCY EXIT DOOR CRACK AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: ANGLE — CORRODED · airframe 30,282 hrs · 21,335 cycles

CORROSION ON PAX DOOR FORWARD CAP ANGLE REPLACED PAX DOOR FWD CAP ANGLE.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

LH SIDEWALL SEAT RAIL HAS CORROSION. FS667-FS720. REPLACED SEAT RAIL.

Part: FRAME — CORRODED · airframe 30,282 hrs · 21,335 cycles

IN THE AVIONICS BAY THE FS319 LOWER FRAME SECTOR HAS CORROSION NOTED ON ITS ATTACH FLANGE AND WEB BETWEEN STGR25L AND STGR27. PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-006-A01.

Part: INTERCOSTAL — CORRODED (CORRODED) · airframe 30,282 hrs · 21,335 cycles

AVIONICS DOOR FWD LH LATCH PIN INTERCOSTAL CORRODED.

Part: SEAT TRACK — CORRODED · airframe 30,282 hrs · 21,335 cycles

FLOOR SEAT TRACK LBL9 HAS FRETTING AND CORROSION FS661+32-FS677.00. REPLACED SEAT TRACK.

Part: STRINGER — CORRODED (FS 954-969) · airframe 30,282 hrs · 21,335 cycles

CORROSION FOUND ON STGR 26L BETWEEN FS954 AND FS969. PERFORMED SPLICE REPAIR OF STRINGER REF EA: CRJ953.13833 REV A 6/24/2022..

Part: FRAME — CORRODED · airframe 30,282 hrs · 21,335 cycles

CORROSION FOUND ON WEB AND ATTACH FLANGE AT FS847+32 BETWEEN STGR25L AND 26R. PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-001-A03.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

RH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS865-FS969. REPLACED SEAT RAIL.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

RH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION AT FS847+32-FS865. REPLACED SEAT RAIL.

Part: INTERCOSTAL — CORRODED · airframe 30,282 hrs · 21,335 cycles

IN THE AVIONICS BAY THE INTERCOSTAL TO THE RH SIDE OF STGR 27 BETWEEN FS349 AND FS364 COMMONLY REFERED TO AS STGR 27R HAS CORROSION NOTED ON ATTACH FLANGE . REPLACED INTERCOSTAL.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

LH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS847+16-FS913 REPLACED SEAT RAIL.

Part: SEAT TRACK — CORRODED · airframe 30,282 hrs · 21,335 cycles

LEFT SIDE SEAT TRACK IS CORRODED FS913.00-969.00. REPLACED SEAT TRACK.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

LH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS744.15-FS761.85. REPLACED SEAT RAIL.

Part: SEAT TRACK — CORRODED · airframe 30,282 hrs · 21,335 cycles

SEAT TRACK AT LBL9, FS581-FS661+32 HAS OUT OF LIMITS CORROSION DAMAGE. REPLACED SEAT TRACK.

Part: NONE — CORRODED · airframe 30,282 hrs · 21,335 cycles

LH SIDEWALL SEAT RAIL FS661+16-FS 667.00 IS CORRODED. REPLACED SIDEWALL SEAT RAIL AT FS661+6-FS667.00

Part: PANEL — CHAFED · airframe 30,282 hrs · 21,335 cycles

PANEL 684AB IS CHAFED. PANEL REPLACED.

Part: PANEL — CHAFED · airframe 30,282 hrs · 21,335 cycles

LEFT INBOARD FLAP LEADING EDGE PANEL 584GB IS CHAFFED. LOCATED, DRILLED, AND INSTALLED NEW PANEL 584GB PER CRJ SRM 51-40-11-001-001-A01

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 27,993 hrs · 19,240 cycles

MID-CABIN OVERHEAD EXIT LIT WITH BOTH EMERGENCY LIGHT SWITCHS IN OFF POSITION. R & R BATTERY CHARGER ASSY, IAW AMM 33-51-17 P/N ON/OFF 11-0049 S/N OFF 23668 S/N ON 26709. OPERATIONS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 23,804 hrs · 15,912 cycles

INTEMITENT FWD LAV SMOKE MASTER WARNING IN FLIGHT. FLIGHT ATTENDENT VERIFIED NO SMOKE IN LAV IN FLIGHT. R&R FWD LAV SMOKE DETECTION IAW AMM 26-16-01, OPS CK GOOD P/N OFF ON 474560-46 S/N OFF TJA0563 S/N ON TJA0529.

Part: OXYGEN MASK — LOOSE (COCKPIT) · airframe 23,713 hrs · 15,843 cycles

AFTER CHANGING O2 UNIT ON PREVIOUS WRITE UP, AIRCRAFT SHOWED APPROX 174. DURING FLIGHT NOTICED O2 AT 1040 AND DROPS APPROX 10 PSI EVERY COUPLE MIN. OXY LOW PRESS CAUTION ON FAIL AT GATE 880PSI. FOUND FO'S BOX AND MASK LOOSE REINSTALLED FO'S BOX AND MASK REF MM 35-11-12. SERVICED CREW O2 REF AMM 12-16-35 TO 1625 PSI A/C OK FOR SERVICE.

Part: STOWAGE BOX — INOPERATIVE (COCKPIT) · airframe 23,713 hrs · 15,843 cycles

FO SIDE O2 MASK PUSH TO TEST BUTTON INOP. REMOVED AND REPLACED THE FO STOWAGE BOX IAW TECHNICAL SUPPLEMENT 001820. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.

Part: UNKNOWN — ODOR (MAIN CABIN) · airframe 23,208 hrs · 15,468 cycles

DURING DESENT, A STRONG OIL ODOR WAS COMING FROM THE VENTS, THROUGHOUT CABIN & FLIGHT DECK. BLEEDS NORMAL & OOF OF ENGINES. ODOR DISSIPATED AFTER BLEEDS TRANSFERED TO APU. PERFORMED AN OPS CHECK OF THE LT AND RT PACKS WITH ENGINES AS BLEED SOURCE IAW AM 21-50-00-862-805. NO ODORS NOTED, ACFT OK FOR SERVICE.

Part: NACELLE — CONTAMINATED · airframe 230,208 hrs · 15,468 cycles

AFTER ENGINE START AND DURING FLIGHT, A STRONG OIL ODOR FROM THE A/C PACKS, ODOR IN THE COCKPIT & AFT ROWS. RAN ENGINES IAW AMM 71-00-00. RAN PACKS IAW 21-51-00. OPENED THE ENGINE COWLS AND FOUND RESIDUAL OIL. CLEANED IAW SRM 51-26-00. NO DEFECTS FOUND. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 23,132 hrs · 15,411 cycles

RIGHT SIDE MIDDLE EMERGENCY LIGHT WAS OUT. REMOVED AND REPLACED RIGHT SIDE MIDDLE EMERGENCY LIGHT, LIGHT REMAINS INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,048 hrs · 15,343 cycles

CABIN EMERGENCY LIGHTS DS154, DS156, AND S342 WERE INOPERATIVE. REMOVED AND REPAIRED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-21-17, OPS TESTED GOOD IAW AMM 33-51-17-710-801.

Part: FORMER — CORRODED (PASSNEGER DOOR) · airframe 23,048 hrs · 15,343 cycles

MAIN DOOR HAD CORROSION AROUND FWD LOWER TENSION LATCH. REMOVED AND REPLACED THE FWD FORMER ON THE PAX DOOR IAW SRM 51-42-06, AND SRM 51-42-21.

Part: HANDLE — CRACKED (PASSENGER DOOR) · airframe 23,048 hrs · 15,343 cycles

THE PAX DOOR INNER HANDLE WAS CRACKED AT THE MOUNT POINT. LOCATED & DRILLED A NEW HANDLE IAW SRM 51-40-11, INSTALLED THE HANDLE IAW WC 6273079, 1015659 8000-0074.

Part: ANGLE — CORRODED (PASSENGER DOOR) · airframe 23,048 hrs · 15,343 cycles

MAIN DOOR, FWD SIDE ANGLE BRACKET BELOW THE HINGED STEP WAS CORRODED. REMOVED & REPLACED THE TOP WEB PANEL IAW SRM 51-42-06, AND 51-42-13.

Part: SKIN — CORRODED (PASSENGER DOOR) · airframe 23,048 hrs · 15,343 cycles

MAIN DOOR FWD SIDE LOWER ACCESS DOOR CORRODED AROUND EDGE. REMOVED & REPLACED THE INNER DOOR SKIN WITH NEW FABRICATED SKIN IAW SRM 51-42-06, AND 51-42-13.

Part: WEB — CORRODED (PASSENGER DOOR) · airframe 23,048 hrs · 15,343 cycles

MAIN ENTRANCE DOOR, FWD SIDE LOWER STAIR ACCESS PANEL FRAME AREA WAS CORRODED. REMOVED & REPLACED THE FWD SIDE RISER WEB IAW SRM 51-42-06, AND 51-42-13.

Part: BRACKET — CRACKED (E/E BAY) · airframe 23,048 hrs · 15,343 cycles

JB-6 SUPPORT BRACKET WAS CRACKED AT THE NUTPLATE. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06, AND 51-40-11.

Part: WEB — CRACKED (BS 192) · airframe 23,048 hrs · 15,343 cycles

WEB AT BS 192, WL 79.5, RT SIDE AT ADG PUMP WAS CRACKED. REPAIRED THE WEB IAW SRM 53-11-43-201-001-A01.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,944 hrs · 15,256 cycles

DURING DESCENT STRONG MILDEW ODOR THRU PACKS WITH LOW PSI 20. RAN PACK BOTH HOT AND COLD NO ODOR NOTICED IAW AMM 21-50-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,606 hrs · 14,992 cycles

A/C PACKS HAVE A FOUL ODOR. PERFORMED AN OPS TEST OF AIR CONDITIONING SYS WITH APU AND ENGINES IAW AMM 21-51-00. OPS CHECK GOOD. RAN THE LT & RT PACKS FOR OVER 1 HOUR. SUSPECT DE ICE FLUID INGESTION. ODOR IN COCKPIT DISAPPATED.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 22,541 hrs · 14,943 cycles

EXIT SIGN DETACHED. INSTALLED THE SIGN, NO DEFECTS NOTED IAW AMM 33-51-07.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 22,364 hrs · 14,822 cycles

DURING APPROACH, APPROX 12,000 FT, RECEIVED AN EICAS FOR THE FWD LAVATORY SMOKE WARNING, FOLLOWED ABOUT 15 SECONDS LATER BY AN AFT LAV SMOKE WARNING. . COMPLETED EMERGENCY CHECKLIST & QRH. NO VISIBLE SMOKE OR ODOR WAS DETECTED. ALARM CEASED ON OPENING THE PAX DOOR AT THE GATE. FALSE INDICATION. CHECKED MDC FOR MESSAGES NONE PRESENT. REPLACED FWD AND AFT LAV SMOKE DETECTORS IAW AMM 26-16-01, OPS CHECKED GOOD.

Part: SMOKE DETECTOR — ACTIVATED (FWD LAVATORY) · airframe 22,309 hrs · 14,786 cycles

SMOKE FWD LAVATORY WARNING MESSAGE. FOUND THE CIRCUIT BREAKER OPEN FOR THE LAVATORY FAN, RESET AND CLOSED BREAKER FOR THE LAVATORY FAN. PERFORMED TEST OF THE LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CHECKED GOOD. OK FOR SERVICE

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,307 hrs · 14,784 cycles

AFT FACE OF CREW STORAGE FLOOD LIGHT BULBS BURNT OUT. CONNECTED P337 TO J337 BEHIND GALLEY G2, RELAMPED D85515 AND D5159 FLOOR LEVEL EMERGANCY FLOOD LIGHTS. OPERATIONAL TEST OF THE FLOOR LEVEL EMERGANCY FLOODLIGHTS CHECKS GOOD IAW CRJ900 AMM 33-51-11-000- 801 (AO1) 33-51-11-400-801 (A01) 33-51-00-710-802 (A03)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,307 hrs · 14,784 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01 TYPE II.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 20,957 hrs · 13,731 cycles

HI-PRESSURE CONNECTION BOX INVOLVED IN PULL AWAY INCIDENT. REMOVED, FABRICATED AND INSTALLED STRINGER 17L RE-INFORCEMENT ANGLE IAW EC/TC EO 900-53-00-00001 REV O AND DRAWING NR CC670-35171 REV C.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,910 hrs · 13,700 cycles

DURING MAINTENANCE INSPECTION, THE EXTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,883 hrs · 13,685 cycles

THE CREW REPORTED EMERGENCY LIGHT ON RIGHT SIDE OF SERVICE DOOR NEAR THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL CHECKED GOOD.

Part: FAN — FAILED (LAVATORY) · airframe 20,554 hrs · 13,458 cycles

AFT LAV SMOKE WARNING FLIGHT FL 240. REMOVED AND REPLACED LAV EXHAUST FAN IAW AMM 21-23-93 IPC 21-23-93 ITEM 5 . OPS CK GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 18,506 hrs · 12,021 cycles

2 SMALL AREAS OF EMERGENCY GLOW IN THE DARK STRIPS ARE MISSING IN FRONT. REPLACED MISSING EMERGENCY FLOOR PATH MARKING, PHOTOLUMINESCENT IN THE FRONT GALLEY IAW AMM 33-51-01, ACFT GOOD TO RETURN TO SERVICE.

Part: SIGN — MISSING (CABIN) · airframe 17,669 hrs · 11,447 cycles

OVERHEAD EXIT SIGN AT ROW 13 MISSING. REINSTALLED OVERHEAD EXIT SIGN AT CENTER AISLE SEAT ROW 13, REF AMM 25-61-00.

Part: LIGHT — MISSING (CABIN) · airframe 17,250 hrs · 11,155 cycles

EMERGENCY LIGHT FRONT OF CLOSED F/A REPORT MISSING. INSTALLED NEW FLOOR LIGHTING STRIP ON FLOOR IAW AMM 25-25-00. ACFT OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,954 hrs · 10,931 cycles

EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS IAW AMM 33-51-11.

Part: MEGAPHONE — NOT REPORTED (CABIN) · airframe 16,633 hrs · 10,694 cycles

CABIN MEGAPHONE REQUIRES REPLACEMENT. R & R MEGAPHONE IAW AMM 25-61-14 AND AIPC REF. 25-61-14, FIG 1, ITEM 5.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 15,880 hrs · 10,181 cycles

AFT EMERGENCY LIGHT ON THE RT OVERWING IS INOPERATIVE. REMOVED RT OVERWING EXT EMERGENCY LIGHT DS101 FOUND WIRE PULLED FROM PIN. REPINNED WIRE IAW ESPM 20-16 REINSTALLED LIGHT ASSY WIRE. T/S SYSTEM AND FOUND POSITIVE WIRE PULLED OUT OF THE BACK OF THE LIGHT ASSY RESEATED PIN AND PERFORMED OPS CHECK OF THE LIGHT. OPS CHECK OF THE LIGHT ASSY WAS GOOD AT THIS TIME IAW AMM 33-51-15-710-801-A01.

Part: SPRING — MALFUNCTIONED (PAX DOOR) · airframe 15,880 hrs · 10,181 cycles

PASSENGER DOOR FAILED FUNCTIONAL CHECK. R & R FWD GAS SPRING OF THE FWD COUNTER BALANCE SYSTEM IAW AMM 52-11-17-000-801 AND 52-11-17-400-801-A01. OPS AND FUNCTIONAL TEST GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LGIHTS) · airframe 15,880 hrs · 10,181 cycles

OPS TEST OF THE EMERGENCY LIGHT FAILED. FOUND NR 1 EMERGENCY BATTERY PACK TO BE UNSERVICABLE REF-AMM 33-51-17-000-801, A01 AND 33-51-17-400-801, A01. REMOVED BATTERY PACK IAW AMM 33-51-17-000-801, A02, AJPC 33-51-17-ITEM 6 INSTALLED A SERVICEABLE BATTERY PACK IAW AMM 33-51-17-400-801, A02. PERFORMED OPS TEST OF THE EMERGENCY LIGHT AND LIGHTS OPS CHECK GOOD AT THIS TIME IAW AMM 83-51-00-710-802 A03.

Part: STRINGER — CORRODED (BS 437) · airframe 15,880 hrs · 10,181 cycles

FOUND CORROSION ON STR 19R 2" AFT OF FS 437.00. REMOVED CORROSION STR 19R, 2" AFT OF FS437.00, REF: SRM 51-21-06-001-001-A01. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-03-101-007-A02. COMPLIED WITH EA 32-201-096. RECEIVED ECTC EA 32-2015-096 VERIFIED ALL STEPS OF EA 32-2015-096 ARE ACCOMPLISHED COMPLIED WITH ECTC EA 32-2015-96.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 15,880 hrs · 10,181 cycles

CORROSION ON LOWER SILL ANGLE AT SERVICE DOOR FS 314. LWR SILL ANGLE CORRODED OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. R & R LWR SILL ANGLE IAW SRM 51-42-06-001-001-A01. REMOVED ATTACH ANGLE FROM WEB CORRODED BEYOND LIMITS REQUIRE REPLACEMENT IAW SRM 51-42-06-001-001-A01/ 51-21-06-001-001-A01. INSTALLED, 4EA ATTACH ANGLES TO WEB FLOOR PROTECTOR IAW SRM 51-42-06-001-001-A01, NEW PARTS INSTALLED.

Part: SEAT TRACK — CORRODED (BS 661-667) · airframe 15,856 hrs · 10,163 cycles

SEAT TRACK SEGMENT FROM FS5661+32 TO FS677 AND AT LBL9 IS CORRODED OUT OF LIMITS. RECEIVED ECTC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV J AS WRITTEN. REMOVED SENT TRACK SEGMENT FROM FS 661+32- FS.677 AT LBL 9 IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT TRACK SEGEMENT FROM FS661+32- FS677 AT LBL 9 IAW AMM 53-00-49-400-801-A11.

Part: ATTACH FITTING — CORRODED (BS 629) · airframe 15,856 hrs · 10,164 cycles

MID CARGO BAY CARGO ATTACH POINT CORRODED AT FS629 AND APPROXIMATELY STR 23L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. VERIFIED ALL STEPS OF EA 32-2015-094 ARE COMPLETE. COMPLIED WITH ECTC EA 32-2016-094.

Part: FLOOR SUPPORT — CORRODED (BS 314) · airframe 15,856 hrs · 10,163 cycles

CORROSION ON SERVICE DOOR FLOOR SUPPORT ANGLE AT FS 314. CORRODED BEYOND LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED SERVICE DOOR FLOOR SUPPORT ANGLE AT SERVICE DOOR 51-42-06-001-001-A01. INSTALLED SERVICE DOOR FLOOR SUPPORT ANGLE AT SERVICE DOOR FLOOR SILL LOWER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-667) · airframe 15,856 hrs · 10,163 cycles

SEAT TRACK SEGMENT FROM FS5661+32 TO FS677 AND AT RBL9 IS CORRODED OUT OF LIMITS. RECEIVED 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. REMOVED SEAT TRACK SEGMENT FROM FS 661+32 - FS 677 AT RBL 9 IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT TRACK SEGMENT FROM FS 661+32 - FS 677 AT RBL9 IAW AMM 53-00-49-400-801-A11.

Part: SKIN — DAMAGED (BS 661) · airframe 15,856 hrs · 10,163 cycles

LIGHTING STRIKE TEMP FASTENER AT FS 661+62 BETWEEN STRS 12L + 13L. TEMP FASTENER AT FS661 BETWEEN STR 12L + 13L REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01 REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARY REV 53-0050, TYPE 3B PERMANENT REPAIR TASK 57-00-00-201-006-A03 AND RESTORE FINISH IAW SRM 51-21-16. PERFORMED CONDUCTIVITY TEST OF FUSELAGE SKIN IAW SRM 53-00-00-201-003-A03, TR53-0050 CONDUCTIVITY READING IS 33.94 PERCENT IACS READING IS WITHIN LIMITS SRM 51-11-20-001-001-A01 PERFORMED EDDY CURRENT INSPECTION OF FUSELAGE SKIN AT FS 661+32 STR 12L-13L IAW NDTM PT.1, 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 15,856 hrs · 10,163 cycles

CORROSION FOUND ON THE LT WEB AT FS280.00. REMOVED CORROSION FROM WEB AT LBL 11, FS 280 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01, FIG 53-11-10-994-804. RECEIVED AND COMPLIED WITH EA 32-201-085 AS PERMANENT DISPOSITION MAC6MTC 3/9/15, KF, 3/22/15.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,856 hrs · 10,163 cycles

SEAT TRACK SEGMENT FROM FS581 TO FS661+32 AND AT RBL9 CORRODED IN SEVERAL PLACES. RECEIVED AND COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. R & R SEAT RAIL SEGMENT AT FS581, RBL9 IAW AMM 53-00-49-000-801, CONFIG A11 AND 53-00-49-400-801, CONFIG A11.

Part: ANGLE — CORRODED (BS 1000-1047) · airframe 15,856 hrs · 10,164 cycles

CORROSION AROUND ALL NUTPLATE LOCATIONS ON AFT CARGO DOOR SILL PLATE FROM FS 1000 TO FS 1047. DAMAGE ON AFT CARGO DOOR SILL PALTE FOUND TO BE OUT OF LIMITS IAW SRM 53-61-23-101-001-A01. REMOVED AFT CARGO DOOR SILL PLATE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED ALL FASTENER HOLES IN NEW SERVICEABLE LOWER SILL ANGLE, FS 1000-FS 1047 IAW SRM 51-40-11-001-001-A01 AND DWG MM670-35085. INSTALLED ALL CHERRY MAX FASTENERS IAW SRM 51-42-13-001-001-A01 ALL HI LIGHTS IAW SRM 51-42-21-001-001-A01 AND STOP BLOCK NUTPLATES IAW SRM 51-45-00-001-001-A01 AND DWG MM670-35085. REMOVED 3 EA INNER CHORD ANGLES AT FS 1000-FS 1015, FS 1015- FS 1031 AND FS 1031-FS 1047 BELOW LOWER SILL IAW SRM 51-42-06-001-001-A01. INSTALLED 3EA INNER CHORD ANGLES BETWEEN FS 1000 AND FS 1047 BELOW LOWER SILL ANGLE AT LBL 40 IAW SRM 51-42-06-001-001-A01 51-42-21-001-001-A01 AND DWG MM670-35085. REMOVED 2 EA CARGO TIE DOWN SUPPORTS AND 2EA MOUNTING BRACKETS AT LBL 40, FS 1000-FS 1015 FS 1015-FS 1031 IAW SRM 51-42-06-001-001-A01. INSTALLED 2 EA CARGO TIED DOWN SUPPORTS AND MOUNTING BRACKETS AT LBL 40, FS 100 - 1015 AND FS 10015-1031 IAW SRM 51-42-06-001-001-A01 AND DWG MM670-35041.

Part: ATTACH FITTING — CORRODED (BS 557) · airframe 15,856 hrs · 10,163 cycles

FWD CARGO BAY CARGO ATTACH POINT CORRODED AT STR 27 AND LBL 3.4, FS 557. BEGAN REMOVING CORRISION ON FWD CARGO BAY ATTACH POINT AT STRINGS 27 BETWEEN FS 533+549 IAW SRM 51-21-06-001-001-A01. REMOVED REMAINING CORROSION FROM ATTACH POINT IAW SRM 51-21-00-001-001-A01. REMOVED 5EA RIVETS FROM INBD FLANGE OF CARGO ATTACH POINT IAW SRM 51-42-06-001-001-A01. REINSTALLED 5 EACH RIVETS ON INBD FLANGE OF CARGO ATTACH POINT REF: DWG SH690-33600 REV :Y, SRM 51-42-06-001-001-A01.

Part: ATTACH FITTING — CORRODED (BS 565) · airframe 15,856 hrs · 10,163 cycles

FWD CARGO BAY CARGO ATTACH POINT CORRODED AT FS 565 AND AT APPROXIMATELY STR 24L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-093.

Part: SKIN — DAMAGED (BS 847) · airframe 15,856 hrs · 10,163 cycles

LIGHTNING STRIKE TEMP FASTENER AT FS 847+16 BETWEEN STRS 14L + 15L. TEMP FASTENER AT FS 847+16 BETWEEN STRS 14L AND 15L. REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01 REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARY REMOVED 53-0050, TYPE 3B PERMANMENT REPAIR TASK 53-00-00-201-003-A03 AND RESTORE FINISH SRM 51-21-16. PERFORMED CONDUCTUITY TEST OF FUSELAGE SKIN IAW SRM 53-00-00-201-003-A03, TR53-0050 AND NDTM PT 6 53-00-000-252-A01 CONDUCTIVITY READING IS 33.74 PERCENT IACS READING IS WITHIN LIMITS IAW SRM 51-11-20-001-001-A01 PERFORMED EDDY CURRENT INSPECTION OF FUSELAGE SKIN AT FS 847+16, STR 14L-15L IAW NDTM PT 1 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 15,856 hrs · 10,163 cycles

SEAT TRACK SEGMENT FROM BS 581 TO 661+32 AND AT LBL9 CORRODED OUT OF LIMITS RECEIVED & COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV J AS WRITTEN. R & R SEAT RAIL SEGMENT FS 581, LBL9 IAW AMM 53-00-49-000-801, CONFIG A11 & 53-00-49-400-801 CONFIG A11.

Part: ATTACH FITTING — CORRODED (BS 565) · airframe 15,856 hrs · 10,163 cycles

FWD CARGO BAY CARGO ATTACH POINT CORRODED AT STR 27 AND FS 565. DAMAGE WAS FOUND TO BE FAR OUT OF LIMITS. REMOVED BRACKET IAW SRM 51-42-22-001-001-A01 AND 51-42-20-001-001-A01. STARTED LOCATING FASTENER HOLES IN NEW BRACKET IAW SRM 51-40-11-001-001-A01. COMPLETED LOCATION, DRILLING AND DEBURRING HOLES, IN NEW SERVICABLE CARGO BAY ATTACH PAST BRACKET IAW SRM 51-40-11-001-001-A01. DWG SH 690-33600. INSTALLED NEW SERVICABLE FWD CARGO BAY CARGO ATTACH POINT BRACKET ST FS 565 STR 27 IAW SRM 51-42-22-001-001-A01 AND 51-42-20-001-001-A01, DWG SH 690-33600.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,856 hrs · 10,163 cycles

SEAT TRACK SEGMENT CORRODED BETWEEN FS 485 AND FS 581 AT RBL 9. RECEIVED EC/TC REO 670-53-00-343. REMOVED SEAT TRACK AT RBL BETWEEN FS 485- FS 581 IAW AMM 53-00-49-000-801-A01-A11. INSTALLED NEW SEAT TRACK SEGMENT BETWEEN FS 485 AND FS 581 AT RBL 9 IAW AMM 53-00-49-400-801-A11. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV J AS WRITTEN.

Part: SKIN — DAMAGED (BS 913) · airframe 15,856 hrs · 10,163 cycles

BLEND ON COUNTER SINK AT FS 913.00 AND 2.7" BELOW STRINGER 16L REF W/O 299955, N/R 00042 FOUND UPON TEMP FASTENER REMOVAL. MEASURED BLEND AT RIVET COUNTERSINK BLEND MEASURES 0.029", DEEP X 0.350", WIDE X 0.200 LONG DANAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-210-003-A03. RECEIVED & COMPLIED WITH REO 690-53-51-121. COMPLIED WITH REO 690-53-51-121 IAW NDTM PT-1, 51-20-006-250-A01, NO INDICATIONS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED · airframe 15,849 hrs · 10,159 cycles

GALLEY 2 FLOOR TIE DOWN CORRODED ON RBL9 SEAT TRACK. REMOVED CORRODED FITTING AND INSTALLED NEW SERVICABLE FITTING GALLEY NR 2 LOCATION RBL9 IAW SRM 51-41-02-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,849 hrs · 10,159 cycles

FS 280 FWD SUPPORT ANGLE CORRODED OUT OF LIMITS. LOCATED & INSTALLED FS 280 FWD SUPPORT ANGLE IAW DWG NR CC670-34095 & SRM 51-42-06-001-001 & 51-40-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 15,849 hrs · 10,159 cycles

1 EACH FLOORBEAM PACKER CORRODED AT RBL9 AND FS 349. REMOVED CORRODED PACKER AND REPLACED WITH NEW PACKER IAW SRM 51-42-06-001-001-A01.

Part: DOOR FRAME — CORRODED (BS 280) · airframe 15,849 hrs · 10,159 cycles

RIGHT COCKPIT DOOR POST CORRODED AT FS 280 BEAM. BOTTOM OF DOOR POST CORRODED 100 PERCENT MATERIAL LOSS, RBL11, FS280 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-087 P1, STEPS 1 (A-I). RECEIVED ECTC EA 32-2015-087 AND EA 32-2015-087 FINAL. VERIFIED ALL STEPS PREVIOUSLY COMPLIED WITH.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 15,849 hrs · 10,159 cycles

2EA FLOORBEAM PACKERS CORRODED AT RBL9 AND FS 333. R & R 2 EA PACKERS WITH NEW PACKERS IAW SRM 51-42-00-001-001-A01.

Part: DOOR FRAME — CORRODED (BS 280) · airframe 15,849 hrs · 10,159 cycles

LT COCKPIT DOOR POST CORRODED AT FS 280 BEAM. BOTTOM OF DOOR POST CORRODED 100 PERCENT MATERIAL LOSS, RBL11, FS280 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-086 P1, STEPS 1 (A-I). RECEIVED EA 32-2015-086 FINAL. VERIFIED ALL STEPS PREVIOUSLY COMPLIED WITH. COMPLIED WITH ECTC STS EA 32-2015-086 AND VERIFIED ALL STEPS OF STS EA 32-2015-086, REV B WERE COMPLIED WITH.

Part: SKIN — DAMAGED (BS 830-847) · airframe 15,849 hrs · 10,159 cycles

BURNED FASTENERS FROM LIGHTING STRIKE. 1 BURN ON STR 14L BETWEEN FS 830 AND 847. REMOVED FINISH AT TEMP FASTNER IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENER IAW SRM 51-42-12-001-001-A01. COMPLIED WITH SRM TR 53-0050 REPAIR TYPE 3B PERMANENT REPAIR TASK 53-00-00-201-003-A03. REMOVED FINSIH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENER IAW SRM 51-42-12-001-001-A01. COMPLIED WITH SRM TR 53-0050 REPAIR TYPE 3B PERMANMENT REPAIR TASK 53-00-00-201-003-A03. INSPECTED FUSELAGE AREA FOR DAMAGE AT FS 847 BETWEEEN STRS 14L AND 15L. NO DEFECT NOTED AT THIS AREA.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,849 hrs · 10,159 cycles

LEFT INTERCOSTAL BETWEEN FS 349-364 CORRODED. LEFT INTERCOSTAL HAS EXFOLIATING CORROSION OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED LT INTERCOSTAL FROM STA 349 TO 364 LOCATED, DRILLED AND DEBURRED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL LG OF STR 27 FS349-364 REF SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,849 hrs · 10,159 cycles

RIGHT INTERCOSTAL BETWEEN FS 349.00 AND 364 IS CORRODED. RIGHT INTERCOSTAL HAS EXFOLIATING CORROSION AT RADIUS OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED RT INTERCOSTAL FROM STA 349 TO 364 LOCATED, DRILLED AND DEBURRED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL RT OF STR 27 BETWEEN FS349 TO 364 REF SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,849 hrs · 10,159 cycles

FLOORBOARD 141ALF ATTACH ANGLE AT FS 280 IS CORRODED. REMOVED CORROSION FROM SH670-32330-1 ATTACH ANGLE STA 280 IAW SRM 51-21-06-001-001-A01. NO ALLOWABLE DAMAGE LIMITS EFFECTIVE FOR THE ACFT. R & R FLOORBOARD 141ALF ATTACH ANGLE AT FS280 REF: DWG: PL OC 670-34256, REV N, SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01, AND 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,828 hrs · 10,146 cycles

FWD FACE OF FS 280 FLOORBEAM CORRODED BETWEEN RBL9 AND LBL9. UPON FURTHER INVESTIGATION FOUND THE 280 FWD SUPPORT ANGLE CORRODED AND NOT THE 280 FLOORBEAM. FWD SUPPORT ANGLE CORRECTED.

Part: SKIN — DAMAGED (BS 250) · airframe 15,880 hrs · 10,181 cycles

BURNED FASTENERS FROM LIGHTING STRIKE. COMPLIED WITH PERMANENT REPAIR OF BURNED FASTENERS FROM LIGHTING STRIKE IAW SRM 53-00-00 AND EC/TC REO 690-53-11-748. 1 BURNED RIVET AT FS 250.00 BETWEEN STRS 10L AND 19L. REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENER IAW IAW SRM 51-42-13-001-001-A01. RECEIVED REO 690-53-11-748. REQUESTED AND RECEIVED ECTC REO 690-53-11-748 AND COMPLIED WITH ECTC REO 690-53-11-748 BY VERIFYING REO 690-53-11-748 BY VERIFYING REO 690-53-11-748 REV- HAS BEEN ACCOMPLISHED AND ALL STEPS ARE COMPLETE. 1 BURNED RIVET AT FS 661.00 +32 BETWEEN STRS 13L AND 14L. REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01, CJ84817 3/8/15 MAINTENANCE 12 3/8/15. COMPLIED WITH SRM T/R 53-0050, REPAIR TYPE 3B PERMANENT REPAIR TASK 53-00-00-201-003-A03, WA161715 3/12/15 M/A: REF W/O 299955, N/R 00028 1 BURNED RIVET AT FS 661.00+62 BETWEEN STRS 13L AND 14L CJ84817 3/8/15 MAINTENANCE 12, 3/8/15 C/A: INSPECTED FUSELAGE AREA FOR DAMAGE AT FS 661+62 BETWEEN STRS 13L & 14L. NO DEFECTS NOTED AT THIS AREA. FOUND TEMP FASTENER CLOSE TO THIS AREA AT FS 661.00+62 BETWEEN STRS 12L AND 13L. TEMP FASTENER AT BS 661 BETWEEN STR 12L + 13L REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01 REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARY REV 53-0050, TYPE 3B PERMANENT REPAIR TASK 57-00-00-201-006-A03 AND RESTORE FINISH IAW SRM 51-21-16.

Part: SKIN — DAMAGED (BS 913) · airframe 15,880 hrs · 10,181 cycles

BURNED FASTENER AND BURNED SKIN. COMPLIED WITH PERMANENT REPAIR FOR BURNED FASTENER AND SKIN IAW SRM TEMP REV 50-0050, TYPE 3B PERMANENT REPAIR. 2 BURNED RIVETS AT FS 913.00 BETWEEN STR 17L AND 16L. REMOVED FINISH AT TEMP FASTENERS IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENERS (2) IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARY REV 53-0050, TYPE 3B PERMANENT. REPAIR 3 & RESTORED FINISH IAW SRM 51-21-16-001-001. 1 BURN ON SKIN BETWEEN FS 942.00 AND FS 954 BETWEEN STRS 18L AND 19L REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01. REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARY REV 53-0050, TYPE 3B PERMANENT REPAIR TASK 53-00-00-201-003-A03 & RESTORED FINISH IAW SRM 51-21-16-001-001.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 15,549 hrs · 9,979 cycles

PAX DOOR AFT SKIN DAMAGE ON MCO A141547 HAS PROPAGATED PAST THE LIMITS OF REO 690-52-026. CUT OUT DAMAGED SIDE PANEL IAW REO 670-52-11-104, REV E. FABRICATED ALL REPAIR ITEMS- SHIMS AND DOUBLER SRM 51-24-36 AND SRM 51-24-21 IAW REO 670-52-11-104, REV E. DRILLED NEW FASTENER PATTERN IN SKIN, FABRICATED PARTS AND NEW GAS STRUT BEAM TO FULL SIZE MAINTAINING SPECIFIED PITCH AND ED IAW REO 670-52-11-104, REV E, EXCEPT 3 FASTENERS IN BEAM AND DOUBLER ADDRESSED BY REO 670-52-11-811. WET INSTALLED ALL FASTENERS IAW SRM 51-42-06 AND SRM 51-42-21 IAW REO 670-52-11-104, REV E. INSTALLED SHIM UNDER THE GAS SPRING BEAM IAW REO 670-52-11-104, REV E. CONSIDERED MAJOR REPAIR IAW SOP 5702.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 14,460 hrs · 9,272 cycles

FLOOR LIGHT BROKEN AT ROW 1. REPLACED EMERGENCY LIGHT AND COVER IAW AMM 33-51-00.

Part: HINGE — GOUGED (PAX DOOR) · airframe 13,709 hrs · 8,763 cycles

TWO SCRATCHES WERE FOUND AT PAX DOOR HINGE FUSELAGE SIDE AT LUGS 12 AND 14. COMPLIED WITH EC/TC REO 670-53-21-582. BLENDED SURFACE. MAJOR REPAIR IAW GMM 5-3.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 13,562 hrs · 8,663 cycles

MEGAPHONE INOPERATIVE, REPLACED AFT MEGAPHONE IAW AMM 25-61-14, IPC 25-61-14. OK FOR SERVICE.

Part: LIGHT — MISSING (GALLEY) · airframe 12,750 hrs · 8,168 cycles

GALLEY EMERGENCY LIGHT STRIP MISSING. REPLACED MISSING EMERGENCY LIGHT STRIP IAW AMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 11,748 hrs · 7,577 cycles

SECTION OF EMERGENCY LIGHT MISSING AFT OF GALLEY. FOUND AND SECURED EMERGENCY LIGHT IAW SRM 33-51-01.

Part: SKIN — BURNED (BS 847) · airframe 11,397 hrs · 7,333 cycles

BURNED RIVET AT FS 847 BETWEEN S14-15L. REPAIRED IAW SRM 53-00-00. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 847 S14-15L) · airframe 11,397 hrs · 7,333 cycles

BURNED RIVET AT FS 847 BETWEEN S14-15L. REPAIRED IAW SRM 53-00-00. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 661) · airframe 11,397 hrs · 7,333 cycles

ONE BURNED RIVET AT FS 661+32 BETWEEN S13-14L. REPAIRED IAW SRM 53-00-00. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 830.4-847) · airframe 11,397 hrs · 7,333 cycles

BURN ON SKIN S14L BETWEEN FS 830.4 AND 847. REPAIRED IAW SRM 53-00-00. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 661) · airframe 11,397 hrs · 7,333 cycles

ONE BURNED RIVET AT FS 661+62 BETWEEN S13-14L. REPAIRED IAW SRM 53-00-00. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 691-708) · airframe 11,397 hrs · 7,333 cycles

BURN ON SKIN BETWEEN FS 693 - 708, BETWEEN S13-14L. REPAIRED IAW SRM 51-12-00, 51-21-00. MAJOR REPAIR IAW GMM 5-3.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 10,733 hrs · 6,934 cycles

ASD STRUCTURE FOUR INNER ANGLES CORRODED. R & R ANGLES IAW SRM 51-42-06-001-001 AND DWG NR 601R-319034.

Part: WEB — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

MINOR CORROSION ON WEB RBL 9 FS 280. REPAIR IAW REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

FS 280 LT FLOORBEAM CORRODED. INSTALLED NEW LT FS 280 FLOORBEAM IAW SRM 51-42-06-001-001 AND DWG CC670-34010.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

FLOOR SUPPORT AT FS 280 HAS CORROSION. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-42-13-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 274) · airframe 10,733 hrs · 6,934 cycles

COCKPIT FLOORBEAM AT LBL 12 IS CRACKED AT BS 274. REPAIRED IAW REO 690-53-11-491.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,733 hrs · 6,934 cycles

EMERGENCY LIGHT WIRE BROKEN. REPAIRED WIRE IAW ESPM 20-16-00.

Part: FLOORBEAM — CRACKED (BS 274) · airframe 10,733 hrs · 6,934 cycles

COCKPIT FLOORBEAM AT RBL 12 IS CRACKED AT BS 274. REPAIRED IAW REO 690-53-11-491.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,733 hrs · 6,934 cycles

ASD NR 5 STEP EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE IAW ESPM 20-16-00.

Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,733 hrs · 6,934 cycles

COCKPIT FLOOR SUPPORT ANGLE LT SIDE IS CRACKED AT FS 276. INSTALLED NEW LT FLOOR SUPPORT ANGLE FS 265-280 IAW SRM 51-42-06-001-001.

Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,733 hrs · 6,934 cycles

COCKPIT FLOOR SUPPORT ANGLE RT SIDE IS CRACKED AT FS 276. INSTALLED NEW RT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001 AND DWG CC670-33-052.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 10,733 hrs · 6,934 cycles

FLOORBEAM IS CORRODED. INSTALLED NEW FLOORBEAM ANGLE AT FS 280 IAW SRM 51-42-06-001-001 AND DWG CC670-33052.

Part: WEB — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

MINOR CORROSION ON WEB WHERE LBL 9, FS 280. REPAIRED IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 10,733 hrs · 6,934 cycles

SEAT TRACK AT FS 785.15 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 10,733 hrs · 6,934 cycles

SEAT TRACK FS 364.00 RBL 9 CORRODED. REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-49-400-801.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

FS 280, RT CROSSBEAM CORRODED. INSTALL NEW CROSSBEAM IAW SRM 51-42-06-001-001 AND DWG CC670-34010.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 10,733 hrs · 6,934 cycles

SEAT TRACK AT FS 785.15 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 752.5) · airframe 10,733 hrs · 6,934 cycles

LT SIDE SEAT TRACK AT FS 752.5 CORRODED. REPAIRED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 10,733 hrs · 6,934 cycles

RT FLOOR SUPPORT AT FS 280 CORRODED. REPAIRED IAW REO 670-53-21-139.

Part: NONE — NONE (NONE) · airframe 8,196 hrs · 5,367 cycles

MEGAPHONE INOPERATIVE. PERFORMED OPS CHECK OF MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,843 hrs · 5,134 cycles

PAX DOOR AFT DRAG ANGLE CRACKED REINSPECTION. REINSPECTION OF PAX DOOR AFT ANGLE CRACK. REF REO690-52-11-181. CRACK DOES NOT EXCEED. NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 7,766 hrs · 5,095 cycles

WHEN POWER IS TURNED OFF AND EMERGENCY LIGHTS ARE OFF SOME AFT CABIN EMERGENCY LIGHTS REMAIN ON. REPLACED EPSU BATTERY PACK NR 4 IAW AMM 33-51-017 AND IAW AIPC 33-51-17-01. (SDR CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,766 hrs · 5,095 cycles

NR 4 PASSENGER DOOR AFT DRAG ANGLE CRACKED AT THE DOOR ASSIST PULLEY BRACKET, APPROX 1.5" REFER TO DEFECT 379090 FOR REINSPECT. R & R PAX DOOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,172 hrs · 4,775 cycles

RT WING FWD EMERGENCY EXIT LIGHT INOPERATIVE, R & R EPSU BATTERY PACK NR 5 IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,172 hrs · 4,775 cycles

LT WING AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R EPSU BATTERY PACK NR 5 IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 3,882 hrs · 2,678 cycles

THE GLOW IN THE DARK STRIPS IN FIRST CLASS ARE MISSING AND BROKEN. R & R PHOTOLUMINANCE STRIP IAW AMM 33-51-01. ACFT MX READY. (CLOSED)

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 2,094 hrs · 1,509 cycles

PERFORMED OPS TEST OF FA'S MEGAPHONE IAW MM 25-61-14 WITH NO DEFECTS NOTED.

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 2,095 hrs · 1,509 cycles

F/A MEGAPHONE IS INOP. PERFORMED OPS TEST OF F/A'S MEGAPHONE IAW MM 25-61-14 WITH NO DEFECTS NOTED.