N707EV

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,224 hrs · 29,908 cycles

GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT AFTER LANDING IT EXTINGUISHED. (FLT 3200 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,224 hrs · 29,908 cycles

GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT AFTER LANDING IT EXTINGUISHED. (FLT 3200 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26813001 WITH THE FOLLOWING CORRECTIVE ACTION: "GEAR DISAGREE AND GEAR NOT RETRACTING WAS CORRECTED BY MULTIPLE MAINTENANCE ACTIONSDCU1 WAS FOUND TO BE FAULTY, SEE CP 26814243 FOR REMOVAL AND REPLACEMENTLANDING GEAR PROX SENSING HEALTH CHECK WAS PERFORMED AND MULTIPL PROX SENSOR WERE FOUND TO BE FAULTY. SEE CP'S PX02 REF CP 26814354,PX08 CP 26814355, 26830075 , PX09 CP 26814357, 26830063, PX10 CP 26814920, AND PX 11 CP 26814360.PROX SENSING HEALTH CHECK PERFORMED AGAIN WITH THE PROX SENSORS PASSING, SEE CP'S 26839569, 26839593, 26839595, 26839606, 26839610 SEE CP 26839984 FOR REMOVAL AND REPLACEMENT OF MLG SELECTOR VALVE AND PSEUGEAR IS OPS CHECKING GOOD AT THIS TIME"

Part: UNKNOWN — DID NOT STOW (UNKNOWN) · airframe 41,224 hrs · 29,907 cycles

DURING TAKEOFF, TRIPLE CHIME AND GEAR DISAGREE DURING GEAR RETRACTION, NOSE GEAR DID NOT SHOW RETRACTED. COMPLIED WITH QRH PROCEDURE, GEAR DISAGREE MESSAGE DISAPPEARED, THEN SHORTLY THEREAFTER PROX SYS FAULT 1 STATUS MESSAGE APPEARED. SET UP FOR EMERGENCY LANDING, LANDED WITHOUT ANY ISSUES. (FLT 4949 FILED CLOSED)TROUBLESHOT GEAR DISAGREE AND PROX SYS FAULT 1 STATUS MESSAGE IN REFERENCE TO FIM 32-60-00. INTERROGATED MDC AND FOUND B1 CODE 055323 INDICATING DEFECTIVE PSEU. REMOVED AND REPLACED PSEU IN REFERENCE TO AMM 32-61-01. OPS CHECK OF PSEU GOOD. SET AIRCRAFT ON JACKS IN REFERENCE TO AMM 7-11-01. PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECKS IN REFERENCE TO AMM 32-30-00. FOUND NO DEFECTS IN THE OPERATION OF EXTENSION AND RETRACTION OF LANDING GEARS. OPS CHECK GOOD. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,219 hrs · 29,902 cycles

DAMAGE ON RH SIDE OF AIRCRAFT FUSELAGE BETWEEN FS333.00 AND FS349.00, BETWEEN STGR19R AND STGR21RTHIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1156202 AND 1156470 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: NONE — DAMAGED · airframe 38,818 hrs · 27,972 cycles

REF CP 23937463 FOR ORIGINAL DISCREPANCY AND CP23943655 FOR DAMAGE DETERMINATION. FOUND TWO HOLES TO BE ELONGATED WHILE REMOVING THE PAX DOOR AFT SEAL RETAINER THIS DAMAGE HAS BEEN DETERMINED TO BE MAJOR PER GMM 3-26 REPAIR PER REO 670-52-11-1272. (FILED CLOSED) REPAIRED DAMAGE TO THE PAX DOOR OUTTER SKIN AT SEAL RETAINER SUPPORT ANGLE PER INSTRUCTIONS IN REO 670-52-11-1272 REV - DATED 2021-12-05. TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR WAS ALSO COMPLETED IN REFERENCE TO SRM REF CP 239570836 FOR PRIMER AND PAINT OF REPAIRED AREA AND CP 23953556 FOR PRESSURIZATION CHECK OF PAX DOOR.

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 38,468 hrs · 27,705 cycles

SMELL OF ELECTRICAL SMOKE DETECTED AROUND FL220. AT FL280, SMELL INTENSIFIED AND SMOKE SEEN AROUND WINDOW HEAT IN CA SIDE. (FLIGHT 3084) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23560452 WITH THE FOLLOWING CORRECTIVE ACTION: "INSPECTED CA'S SIDE WINDSHIELD HEAT TERMINALS. FOUND TERMINAL LUG LOOSE AND LOCK WASHER MISSING ON TB2. REPLACED MISSING LOCK WASHER AND REPLACED TERMINAL LUG DUE TO DAMAGE FROM ARCING IN REFERENCE TO AMM 56-11-01. SYSTEM OPS CHECK GOOD AT THIS TIME IN REFERENCE TO AMM 30-41-06."

Part: FILTER — OBSTRUCTED (RECIRCULATION) · airframe 38,468 hrs · 27,705 cycles

DURING CLIMB OUT FROM DFW A VERY INTENSE ELECTRICAL BURNING SMELL ENTERED THE FLIGHT DECK. (FLIGHT 3243 - FILED CLOSED) PLEASE REFERENCE AML 743123 PLEASE REFERENCE AML 743125 PLEASE REFERENCE AML 743191 PLEASE REFERENCE AML 743202 PLEASE REFERENCE AML 743219 UPON ARRIVAL TO A/C FLIGHT CREW REPORTED NOTABLE ELECTRIC ODOR FROM CA GASPER WITH PACKS RUNNING ON ENGINE BLEED AIR DURING CLIMB. FLIGHT ATTENDANTS REPORTED NO ABNORMAL SMELL IN CABIN. PREFORMED SMOKE AND / OR ABNORMAL SMELL IN COCKPIT INSPECTION PER FIM 21-21-00-810-806. FOUND LEFT HAND RE CIRCULATION FILTER AND HOUSING TO BE ENGULFED WITH A PLASTIC SHOPPING BAG. REMOVED DEBRIS FROM FILTER HOUSING AND REPLACED FILTER PER AMM 21-22-12, ALSO REMOVED AND REPLACED LEFT HAND RE CIRCULATION FAN AND CHECK VALVE ASSEMBLY PER AMM 21-22-10 DUE TO AIR STARVATION AND PLASTIC CONTAMINATION. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME WITH ENGINE BLEED AT POWER AND LEFT PACK RUNNING AND RE CIRCULATION FANS ON. A/C OKAY FOR RETURN TO SERVICE. (NOTE: REMOVED RE CIRCULATION FAN HAS A FAINT ELECTRICAL BURNING SMELL TO IT).

Part: DOUBLER — CRACKED (LT TRANS COWL) · airframe 38,394 hrs · 27,646 cycles

LH UPPER TRANS COWL €“ POSSIBLE CRACK ON DOUBLER FOR FWD LATCH CUTOUT (FILED CLOSED) REMOVED AND REPLACED DOUBLER FOR FWD LATCH CUTOUT ON LH UPPER TRANSCOWL IN REFERENCE TO CRJ 700 SRM 51-42-13

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 37,726 hrs · 27,146 cycles

WHILE ON LEFT DOWNWIND, THE SMOKE AFT LAV WARNING LIGHT ILLUMINATED. WE ELECTED TO LAND AND THEN RAN THE QRH. NO EVIDENCE OF ANY SMOKE WAS FOUND. RAN THE QRH AND SECURED THE LAV AREA AND TAXIED TO PARKING WITH NO ISSUE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,722 hrs · 27,144 cycles

DURING SCHEDULED MAINTENANCE IN THE GOJET MAINTENANCE FACILITY IN ST LOUIS INT’L AIRPORT, ST. LOUIS, MO (STL) THE FUSELAGE FRAME UPPER SECTOR AT FS 333.00 BETWEEN S-1R AND S-2R WAS FOUND CRACKED. REPAIRED IAW STS ENGINEERING AUTHORIZATION 70-2020-066

Part: BRAKE — DRAGGING (RT MLG) · airframe 37,411 hrs · 26,927 cycles

TYS A/C WAS LANDING WHEN THE RIGHT MAIN OUTBOARD TIRE BLEW OUT. MAINTENANCE FOUND THE NR 4 BRAKE TO BE DRAGGING. MAINTENANCE REMOVED AND REPLACED THE NR 4 BRAKE ASSEMBLY IAW AMM 32-43-26. REPLACED BOTH TIRES AND WAS RELEASED BACK TO SERVICE AFTER OPS CHECK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,578 hrs · 26,210 cycles

PILOT REPORTED OVERHEAD EMERGENCY LIGHTS AT ROWS 9 AND 15 WERE INOPERATIVE. REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,700 hrs · 24,001 cycles

DURING C CHECK, FOUND FLOORBEAM ANGLE CORRODED BEYOND LIMITS AT FS 280. REMOVED AND REPLACED FLOOBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-25-16-001-001-A01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,733 hrs · 24,040 cycles

CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN ON. THE EMERGENCY LIGHT SYSTEM WAS CHARGED AND FAULT NO LONGER EXIST. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED · airframe 32,797 hrs · 23,272 cycles

WHILE WORKING INTERCOSTAL REPAIR AT FS 280, FS 265, RBL1, FOUND FWD JACK FITTING TO BE CRACKED. REMOVED LT & RT ANGLE FROM FS 280.00 AND FROM LT & RT SUPPORTS BETWEEN FS 265.00 & FS 280.00 REF: SRM 51-42-21-001-001 A01 PART REMOVED TO FOM RT ANGLE AT RBL1- FS 280 WAS FOUND TO HAVE CRACK DAMAGE BEYOND LIMITS REF: SRM 53-00-00-101-001-A01, STARTED DRILLING UP SERVICEABLE RBLA ANGLE & INTERCOSTAL BETWEEN FS 265-FS 280 REF SRM 51-40-11-001-001 A01 AND JACK PAD PAD FITTING & DWG, CC620-32050. COMPLETED DRILLING UP SERVICEABLE RBL-1 ANGLE & INTERCOSTAL BETWEEN FS 280 IAW SRM 51-40-11-001-001 A01 OK OT INSTALL AND JACK PAD FITTING. INSTALLED NOSE JACK PAD, FITTING RBL-1 INTERCOSTAL & ATTACH ANGLE REF SRM 51-42-21-001-001 A01 & DWG CC670-32050. INSTALLED HELI-COIL IN FWD JACKPAD & SEALED AROUND CUTOUT IN FUSELAGE IAW AMM 51-41-10-960-801 A01, 51-23-00-390-809 A01.

Part: SUPPORT — CRACKED (BS 101) · airframe 32,797 hrs · 23,272 cycles

DURING REPAIR OF AFT BAGAGE BAY DOOR SILL STRUCTURE FOUND THE MACHINED FITTING SUPPORTING THE SILL AT FS101.5, CRACKED. REMOVED MACHINED FITTING . FITTING SPLICE, AND STRINGER CLIP IAW SRM 51-42-21-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICABLE MACHINED FITTING IAW SRM 51-40-11-001-001-A01 AND SLATED INSTALLATION IAW SRM 51-42-21-001-001-A01 DWG MM670-35085 DWG MM670-35041 AND INSTALLED SAME SERVICABLE SPLICE IAW SRM 51-42-21-001-A01 AND DWG. FINISHED INSTALLING FASTENERS AT FS 1015 MACHINED FITTING AT LBL35-LBL 45 & INSTALLED CLIP STR18L REF SRM 51-42-21-001-001 & DWG MM67035085, REV L.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 32,797 hrs · 23,272 cycles

AVIONICS BAY DOOR SEAL RETAINER AREAS HAS EXFOLICATED CORROSION. REMOVED DOOR SEAL, DAMAGED IAW AMM 52-42-07-000-801-A01. INSTALLED NEW AVIONICS DOOR SEAL IAW AMM 52-42-07-400-801-A01. REMOVED 4 EA CORRODED SEAL RETAINERS IAW 51-42-06-001-001-A01. INSTALLED 4 EA NEW SEAL RETAINERS IAW SRM 51-42-06-001-00-A01.

Part: FLOOR SUPPORT — CORRODED (BS 761-785) · airframe 32,797 hrs · 23,272 cycles

CORROSION FOUND ON LT FLOOR SILL AT FS 761.93 & 785.07. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2016-079. RECIEVED & COMPLIED WITH EC/TC EA 32-2016-079.

Part: FRAME — CORRODED (BS 549) · airframe 32,797 hrs · 23,272 cycles

CORROSION WAS DISCOVERED ON LT FUSELAGE FRAME 549 BELOW FLOOR SILL. RECEIVED REO 670-53-31-367. REO 53-31-367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: INTERCOSTAL — CORRODED (BS 265-280) · airframe 32,797 hrs · 23,272 cycles

INTERCOSTAL RBL1 FS 280-265 HAS CORROSION, AT NOSE JACK FITTING. REMOVED INTERCOSTAL RBL1, BETWEEN FS 265.00 AND 280.00, REF SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. STARTED DRILLING UP NEW RBL-1, INTERCOSTAL FS 280- FS 265 REF SRM 51-40-11-001-001-A01, DWG CC670-32050. INSTALLED DRILING UP RB2-1 INTERCOSTAL FS 265-280 REF SRM 51-40-11-001-001 AND DWG CC670-32050. INSTALLED RBL-1 INTERCOSTAL REF DWG CC620-32050.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 32,797 hrs · 23,272 cycles

CORROSION FOUND ON RBL9 FLOORBEAM AT FS 1015.00, SAND 1031.00. REMOVED CORROSION ON RBL9, FLOORBEAM AT FS 1015.00 AND 1031.00 IAW SRM 51-21-06-001-001 A01. REPAIRED FLOORBEAM IAW SRM 53-00-41-201-001-A01-GIG 53-00-41-991-830 & EO 700-53-0309, REV 0. STARTED FABRICATING NEW SECTION OF FLOORBEAM RBL 9, FS 1015.00 - FS 1031.00. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-41-991-830.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 32,797 hrs · 23,272 cycles

INTERCOSTAL CORRODED FS 349-364, RBL2. REMOVED INTERCOSTAL AT 349-364, RBL2 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. DRILLED NEW INTERCOSTAL IAW SRM 700 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1031) · airframe 32,797 hrs · 23,272 cycles

CORROSION FOUND ON LBL 27 FLOOR SUPPORT AT BS 1000, 1015, 1031. REMOVED CORROSION ON LBL27, FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01. REPAIRED FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01. FIG 53-00-41-991-830 & EO 700-53-03-08, REV 0.

Part: INTERCOSTAL — CORRODED (BS 265-280) · airframe 32,797 hrs · 23,272 cycles

INTERCOSTAL LBL1 FS 280-265 HAS CORROSION, NOSE JACK FITTING. REMOVED INTERCOSTAL SUPPORT LBL1 BETWEEN FS280.00 AND FS265.00 REF SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-0001-001-A01. STARTED DRILLING UP SERIVCABLE INTERCOSTAL AT LBL1 BETWEEN FS 265-FS280, REF SRM 51-40-01-001-001-A01 AND DWG CC670-32050. COMPLETED DRILLING UP SERIVCEABLE INTERCOSTAL BETWEEN FS265-FS280 IAW SRM 51-40-11-000-001. INSTALLED LBL1 INTERCOSTAL AT FS265-FS280 REF SRM 51-42-06-001-001-0A1 AND DWG CC670-32050.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 32,797 hrs · 23,272 cycles

AVIONIC BAY CRAWL WAY FLOOR SUPPORT HAS CORROSION AT FS 280. REMOVED CORRODED CRAWLWAY SUPPORT IAW SRM 57-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW CRAWLWAY SUPPORT IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, DWG CC670-34256.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 32,797 hrs · 23,272 cycles

INTERCOSTAL CORRODED FS 349-364, LBL2. REMOVED INTERCOSTAL AT 349-364 LBL2 IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01. DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001, A01 & 51-42-21-001-001 A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01. OPS CK CW MAIN AVIONINS DOOR IAW AMM 52-2-00-710-801, A01, OPS CK GOOD.

Part: STRUCTURE — CORRODED (BS 333) · airframe 32,797 hrs · 23,272 cycles

PACKER CORRODED AT RBL 9, FS 333.00. R & R PACKER AT RBL 9, FS 333.0 IAW AMM 51-42-06-001-001 A01.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 32,797 hrs · 23,272 cycles

CORRISON FOUND ON LBL 9, FLOORBEAM AT FS 1031.00. REMOVED CORROSION ON LBL9 FLOOR BEAM AT FS 1031.00 IAW SRM 51-21-06-001-001, A01. REMOVED DAMAGED SECTION OF FLOORBEAM & TRIMMED TO FIT NEW SECTION OF FLOORBEAM, FS 1031, LBL9 REF REO 670-53-00-029 AND EC/TC EO 700-53-0307. COMPLETED FABRICATION & REPAIR OF FLOORBEAM IAW SRM 53-00-41-201-001, A01. FIG 53-00-41-991-830 NR COMPLIED WITH EO 700-53-0307.

Part: FRAME — CORRODED (BS 349) · airframe 32,797 hrs · 23,272 cycles

349 FRAME HAS CORROSION LBL2-STR 26R. REMOVED RT SIDE SEAT RAIL AT FS 565-677 IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT RAIL AT FS 565-677 IAW AMM 53-00-49-400-801-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: SUPPORT — CRACKED (LT WING) · airframe 32,797 hrs · 23,272 cycles

CRACK FOUND ON LT AFT WING TO FUSELAGE FAIRING SUPPORT DIAPHRAGM LBL17.63, FS 923.00. REPAIRED WING TO FUSELAGE AFT FAIRING SUPPORT FS 909.00, LBL 17.63 OR RBL 17.63 IAW REO 670-53-82-478, REV A.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 32,797 hrs · 23,272 cycles

RT SIDE SEAT RAIL, FS 708-FS 761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 32,797 hrs · 23,272 cycles

AFT BAGGAGE BAY DOOR SILL HAS CORROSION. INSTALLED CENTER CARGO TIE DOWN ASSY REF SRM 51-42-06-001-001-A01. INSTALLED 1EA CLIP AT FS 1015 & FS 1031 REF SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & DWG MM670-35085, REV L, POST MOD. STARTED LOCATING FASTENER HOLES IAW SRM 51-40-11-001-001, A01 AND DWG MM670-35085. INSTALLED FWD AND MID INNER CHORDS IAW SRM 51-42-06-001-001-A01 AND DWG MM670-35085, REV L SEE ITEM 12 BELOW FOR AFT CHORD. PICKED UP ALL REMAINING FASTENER HOLES AND COUNTERSUNK AS REQUIRED REF 700 SRM 51-40-11-001-001 & DWG MM670-35085. INSTALLED SHIM AT FS 1000 LBL42, WL73 IAW SRM 51-42-21-001-001-A01 AND DWG MM670-35085, FS 1047 NOT REQUIRED SEE ITEM NR 12 BELOW. PRODUCTION PART UNAVAILABLE AT THIS TIME, THD HAS ISSUED SNIEO MM670-35670, S02 FOR FABRICATION OF MM670-35670-S0201. FABRICATED INNER CHORD, PN, MM 670-35670-S0201 IAW SNIEO MM 670-35670 S02 REF EC/TC CARD NR: SNIEO MM670-35670 S02. INSTALLED INNER CHORD, PN MM 670-35670-S0201 IN LIEU OF INNER CHORD MM 670-35670-003 IAW SNIEO MM 670-35085 S12 NOTE: SHIM AT FS 1047 NOT REQ PER NOTE 2. INSTALLED SILL ASSY AT FS 1000 - FS 1047 REF SRM 51-42-06-001-001-A01 & DWG AMM 670-35085, REV L POST MOD. INSTALLED FWD TIE DOWN ASSY IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, DWG MM670-25041. OPS CK C/W FOR AFT CARGO DOOR.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT LBL9 FS 581-677 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02 & 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 32,797 hrs · 23,272 cycles

RIGHT SIDE SEAT TRACK FS 485 - 565 HAS CORROSION DAMAGE. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, A02 & AMM 53-00-49-400-801, A02.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 32,797 hrs · 23,272 cycles

LEFT SIDE SEAT TRACK BS 708-761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 32,797 hrs · 23,272 cycles

LEFT SIDE SEAT TRACK BS 677-708 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 32,797 hrs · 23,272 cycles

LT SIDE SEAT TRACK FS 565 - FS 677 HAS CORROSION DAMAGE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M. INSTALLED SERVICEABLE LT SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 32,797 hrs · 23,272 cycles

RIGHT SIDE SEAT TRACK BS 677-708 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-00-801, CONF A02 AND AMM 53-00-49-400-801 A02.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT RBL 9 FS 677-830 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED THE NEW SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 32,797 hrs · 23,272 cycles

LT SIDE SEAT TRACK BS 379-485 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 32,797 hrs · 23,272 cycles

LEFT SIDE SEAT TRACK BS 485-565 HAS CORROSION DAMAGE. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT, RBL 9 BS 485-581 HAS CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 32,797 hrs · 23,272 cycles

RIGHT SIDE SEAT RAIL FS 379-485 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06-001-001-A01, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT, LBL9, FS 677-830 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02 & 53-00-49-400-801-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT RBL 9, BS 364-485 HAS CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT RBL 9, BS 581-677 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A02 & 53-00-49-400-801-A02.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 32,797 hrs · 23,272 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN FROM OUTSIDE HANDLE. PERFORMED ADJUSTMENT OF THE OUTER HANDLE ASSY IAW AMM 52-11-03-820-801, A01. PERFORMED LUBRICATION OF PASSENGER DOOR ASSY IAW AMM 12-20-52-640-808, A01. PERFORMED OPS TEST OF PASSENGER DOOR IAW AMM 52-11-00-710-801, A01, OPS CHECK GOOD. PERFORMED OPS TEST OF THE OUTER HANDLE IAW AMM 52-11-03-710-801 A01. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 32,797 hrs · 23,272 cycles

SEAT TRACK SEGMENT LBL9, FS 485-581 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02 & 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 32,797 hrs · 23,272 cycles

RIGHT SIDE SEAT TRACK FS 565 - FS 677 HAS CORROSION DAMAGE. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,575 hrs · 23,087 cycles

EMERGENCY LIGHT OUT, R & R NR 2 BATTERY CHARGER AS REQUIRED IAW AMM 33-51-17, OPS CHECKED GOOD AT THIS TIME, IPC REF 33-51-17, FIG 1, ITEM 8.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 32,231 hrs · 22,803 cycles

F/A MEGAPHONE QUIT WORKING. PERFORMED OPS CHECK OF F/A MEGAPHONE IAW AMM 25-61-14. OPS CKS GOOD.

Part: BATTERY PACK — DISCHARGED (MEGAPHONE) · airframe 32,164 hrs · 22,749 cycles

MEGA PHONE INOPERATIVE. REMOVED AND REINSTALLED BATTERYS, OPS CK GOOD IAW AMM 25-61-14, ACFT OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 32,074 hrs · 22,674 cycles

MEGAPHONE INOPERATIVE. PERFORMED OPS CHECK IAW AMM 25-61-14. NO DEFECT FOUND.

Part: CONTROL PANEL — FAILED (CABIN PRESSURE) · airframe 31,626 hrs · 22,286 cycles

CAPTAIN ADVISED FL 340, MOMENTARILY CABIN ATL WARNING, CABIN ATL AND AP NORMAL, ALT LIMITER CAUTION MESSAGE, SLIGHT ODOR OF ELECTRONICS ODOR IN CABIN REPORTED BY BOTH F/A AND PASSENGERS EMERGENCY DECLARED DIVERTED TO NEAREST AIRPORT. ENROUTE ACFT DIVERTED DUE TO MAINTENANCE. R & R CABIN PRESSURE CONTROL PANEL IAW AMM 21-33-01, REF AIPC 21-33-01, ITEM 5. REF AFDL A382588 FOR OPS CHECK.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 31,570 hrs · 22,245 cycles

ROW 15, EXIT CEILING LIGHT INOPERATIVE. R & R ROW 15 EXIT CEILING LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,570 hrs · 22,245 cycles

12AB LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,665 hrs · 21,518 cycles

F/A SAID EXIT COVER SIGN IS BROKEN BY GALLEY SERVICE DOOR. REPAIRED EXIT SIGN COVER IAW AMM 33-20-00 NO FURTHER DEFECT NOTED.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 30,297 hrs · 21,222 cycles

F/A REPORTS PAX DOOR VERY DIFFICULT TO OPEN. CLEANED AND LUBED PAX DOOR ROLLERS AND MATING SURFACES IAW AMM 52-10-00. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 28,602 hrs · 19,933 cycles

EMERGENCY LIGHTS FAILED OPS TEST IAW 33-51-00-710-802. FOUND PUSHED PIN IN CONNECTOR DS144J1, PIN 1. RESEATED PIN IAW ESPM 20-26-00. OPS CHECK GOOD IAW AMM 33-51-00-710-802.

Part: LINK — CRACKED (RT WING) · airframe 28,602 hrs · 19,933 cycles

RT REAR-WING SPAR LINK LOWER BEARING CRACKED. WING LINKS R & R.

Part: DOOR FRAME — CORRODED (BS 280) · airframe 28,602 hrs · 19,933 cycles

DOOR FRAME BS 280, RT SIDE LOWER EDGE CORRODED. REMOVED CORROSION IAW SRM 51-21-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-00-00-99-803 AND COMPLIED WITH EC/TC REO 670-53-11-944.

Part: BULKHEAD — CORRODED (BS 280) · airframe 28,602 hrs · 19,933 cycles

BS 280 BULKHEAD AT LOWER WEB LT CORRODED ABOVE CROSSBEAM. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH REO 670-53-11-594, REV

Part: BULKHEAD — CORRODED (BS 280) · airframe 28,602 hrs · 19,933 cycles

BS 280 BULKHEAD AT LOWER WEB RT CORRODED ABOVE CROSSBEAM. T COMPLIED WITH STEPS 1-4 ON REO 670-53-11-594-01.

Part: DOUBLER — CORRODED (BS 297) · airframe 28,602 hrs · 19,933 cycles

CORROSION AROUND ONE RIVET ON TOP OF TCAS DOUBLER AT BS 297 AND STRINGER 27. REMOVED RIVET AND CORROSION IAW SRM 51-42-06 AND 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-21-01. INSTALLED NEW DOUBLER IAW SRM 51-42-06-001-001.

Part: FIRESEAL — LOOSE (APU EXHAUST PIPE) · airframe 28,602 hrs · 19,933 cycles

APU TAIL PIPE AFT FIRE SEAL RIVETS LOOSE. COMPLIED WITH GREO 670-49-81-006 AND ECTC REO 670-49-81-006, REV COMPLIED WITH REO 670-49-81-022. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 295-310) · airframe 28,602 hrs · 19,933 cycles

CORROSION BETWEEN BS 295 - 310 ON STRINGER 26R. BLENDED CORROSION ON STRINGER AND FOUND TO BE OUT OF LIMITS IAW 53-21-03-101-002-A01. R & R STRINGER IAW SRM 51-42-06 AND DUG 670-3130, REV N/C.

Part: STRINGER — CORRODED (BS 295) · airframe 28,602 hrs · 19,933 cycles

CORROSION AROUND ONE RIVET BS 295 ON STRINGER 26R. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-802-A01 AND SRM 51-42-06-001-001-A01. STRINGER FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A01. REMOVED AND REPLACED STRINGER IAW SRM 51-42-A01.

Part: WEB — CORRODED (DOOR SILL) · airframe 28,602 hrs · 19,933 cycles

SERVICE DOOR SILL WEB PROTECTOR ATTACH ANGLE CORRODED SH670-31982-1. OBTAINED NEW AND LOCATED AND DRILL HOLES AS REQUIRE IAW SRM 51-40-11-001-001-A01. OBTAINED NEW ATTACH ANGLE LOCATED AND DRILL HOLES AS REQUIRED IAW SRM 51-40-11-001-001-A01. PROTECTOR ATTACH ANGLE INSTALLED AS REQUIRED IAW SRM 51-42-06-001-001-A01. INSTALLED SILL WEB PROTECTOR ATTACH ANGLE AT SERVICE DOOR LOWER SIDE IAW SRM 51-42-06-001-001-A01.

Part: STRAP — CORRODED (BELLY FAIRING) · airframe 28,602 hrs · 19,933 cycles

AFT BELLY FAIRING STRAP IS CORRODED AND HAS NUMEROUS RIVET HEADS PULLED THROUGH THE STRAP. COMPLIED WITH EC/TC EO700-53-0207. FABRICATION OF THE JOINT STRAP FOR AFT WING TO FUSELAGE FAIRING IS COMPLETED IAW EO 700-53-0207 AND DWG PL CC670-39171 AND MEET ALL THE REQUIREMENTS. COMPLIED WITH CPCP INFORMATION FORM IAW SRM 51-20-0-001-001-A01.

Part: STRINGER — CORRODED (BS 317-333) · airframe 28,602 hrs · 19,933 cycles

CORROSION BETWEEN BS 317 - 333 STRINGER 26R. BLENDED CORROSION IAW 51-21-06-001-001-A01. STRINGER FOUND TO BE OUT OF LIMITS IAW SRM 53-21-53-101-002-A01. R & R STRINGER IAW SRM 51-42-06 AND DUC 670-3130, REV N/C.

Part: STRIKER — CORRODED (DOOR SEAL) · airframe 28,602 hrs · 19,933 cycles

SERVICE DOOR, LOWER SEAL STRIKER AROUND FASTEMER HOLES. BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-002. REMOVED SERVICE DOOR FITTING SAL STRIKER IAW SRM 51-42-06. RECEIVED NEW SERVICEABLE SERVICE DOOR FITTING SEAL STRIKER LOCATED DRILLED AND DEBURRED NEW HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-42-06-001-001-A01. REMOVED SERVICE DOOR PROTECTOR PLATE TO FOM IAW AMM 53-21-23-000-801-A01. INSTALLED SERVICE DOOR PROTECTOR PLATE IAW AMM 53-21-23-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,602 hrs · 19,933 cycles

FLOORBEAM ANGLE AT BS 280 IS CORRODED. REMOVED OLD ANGLE, DRILLED & ATTACHED NEW ANGLE IAW SRM 51-40-00-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,601 hrs · 19,932 cycles

BS 280 FLOORBEAM CORRODED ON LT AND RT SIDES. FLOORBEAM R & R IAW SB 670BA-53-041 REV D. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,602 hrs · 19,933 cycles

FLOORBEAM ANGLE AT BS 280 CORRODED. CORROSION DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00-001-001. FLOORBEAM ANGLE R & R IAW SB670-53-041, REV D. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 28,601 hrs · 19,932 cycles

LEFT ENGINE LOWER INBD CASCADE IS CRACKED. REMOVED LT LOWER INBD CASCADE IAW AMM 78-34-01-000-801. INSTALLED LT LOWER INBD CASCADE IAW AMM 78-34-01-400-801-A01 AND SUPPLEMENT 78-34-01, IPC 78-34-01 NR 35A. RECEIVED AND COMPLIED WITH ECTC SB A670BA-78-001, REV A, COMPLIED WITH CLOSE OUT STEPS SA-E IAW AMM 78-34-01-400-801. MAJOR REPAIR-SDR CLOSED.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 28,602 hrs · 19,933 cycles

PASSENGER DOOR SILL CORRODED. R & R DOOR SILL IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — CHAFED (RT NACELLE) · airframe 28,601 hrs · 19,932 cycles

RT LOWER CORE COWL INTERIOR AT 6:00 O'CLOCK POSITION IS CHAFED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ALL STEPS OF REO 670-54-23-959 REV 8. COMPLIED WITH EC/TC REO 670-54-23-959 COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959.

Part: SCREW — SHEARED (THRUST REVERSER) · airframe 28,601 hrs · 19,932 cycles

RT LOWER TRANSCOWL TRACK NYLON INSERTS, INBD AND OTBD ATTACH SCREWS ARE SHEARED OFF. INSTALLED NEW HARDWARE ON RT LWR INBD AND OTBD NYLON INSERT TRACK AREAS IAW REO ECTC 670-54-21-1172. REMOVED RT LWR INBD CASCADE TO ACCESS STUCK SCREW SHANKS IAW AMM 78-34-01-000-802. INSTALLED RT LWR CASCADE INBD PANAL IAW AMM 78-34-01-400-802-A01. RECEIVED ECTC REO 670-54-21-1172. RECEIVED ECTC SBA 670BA-78-001, REVA. COMPLIED WITH EC/TC REO 670-54-21-1172 AND GREO 670-54-21-1172, REV NC DATED 03/12/2013 AS WRITTEN.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 28,601 hrs · 19,932 cycles

SERVICE DOOR SILL CORRODED. SERVICE DOOR SILL LOWER FITTING ANGLE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-001. REMOVED SERVICE DOOR-DOOR STOPS BY REMOVING 12EA BOLTS AND NUTS IAW SRM 51-41-02. REMOVED SERVICE DOOR FLOOR SILL IAW SRM 51-42-06. RECEIVED NEW SERVICEABLE DOOR FLOOR SILL LOCATED. DRILLED AND DEBURRED NEW HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED LOWER ATTACH ANGLE AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,391 hrs · 19,769 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 27,758 hrs · 19,335 cycles

AFT F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IN AFT F/A FLASHLIGHT IAW AMM 25-60-00.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 27,758 hrs · 19,335 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED F/O FLASHLIGHT BATTERIES IAW AMM 25-60-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,628 hrs · 19,244 cycles

NR 6 EXTERIOR EMERGENCY LIGHT IS OUT. REPLACED LAMP IAW AMM 33-51-015, OPS CHECKED GOOD.

Part: FLOORBOARD — DETERIORATED (COCKPIT) · airframe 27,161 hrs · 18,920 cycles

COCKPIT CENTER ENTRANCE FLOORBOARD IS SPONGY. COMPLIED WITH GREO 670-53-00-365. MAJOR REPAIR IAW GMM 5-3.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,771 hrs · 18,639 cycles

F/A REPORTS AFT FLASHLIGHT INOPERATIVE. R & R FASHLIGHT BATTERIES IAW AMM 25-60-00, NO FURTHER DEFECT NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,625 hrs · 18,533 cycles

EXTERIOR EMERGENCY LIGHT AFT OF OVERWING EXIT DOOR IS OUT. R & R LT EXTERIOR EMERGENCY LIGHT AFT OF OVERWING EXIT IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: SENSOR — UNSERVICEABLE (ENGINE OIL TEMP) · airframe 26,043 hrs · 18,089 cycles

LEFT ENGINE OIL TEMP WENT TO 190C. FOLLOWED QRH PREFORMED PRECAUTIONARY SHUT DOWN. DIVERTED. R & R LT ENGINE OIL LEVEL/OIL TEMP SENCOR IAW AMM 79-31-01, REF 79-31-01-01, FIG 1, PREFORMED OPS CHECK IAW AMM 79-30-00 SYS OPS CKD GOOD ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,408 hrs · 17,614 cycles

INTERIOR CEILING EMERGENCY LIGHT OUT AT 9 ABCD. LAMPED INTERIOR CEILING LIGHT AT 9 ABCD IAW AMM 33-51-09.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,163 hrs · 16,646 cycles

SECOND FROM AFT CENTER CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED THE SECOND FROM AFT CENTER CEILING EMERGENCY LIGHT AS REQUIRED AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: CABLE — OUT OF RIG (ELEVATOR) · airframe 23,967 hrs · 16,492 cycles

ELEVATOR RESTRICTED NOSE DOWN. NOSE DOWN NORMAL, NOSE DOWN VERY DIFFICULT. ELEVATOR APPEARS TO BE OPERATING ASSYMETRICALLY. EMERGENCY DECLARED. INSPECTED ELEVATOR CONTROL SYS BY PERFORMING ELEVATOR CONTROL CIRCUIT TENSION CHECK IAW AMM 27-31-00-220-812. FOUND CABLES TO BE WITHIN AMM LIMITS BUT OUT OF RIG WITH TENSION REGULATOR LOCKKBARS INSTALLED & RIG PINS AT TENSION REGULATORS AND AFT CABLE QUADRANTS SL7318. RE-RIGGED LT AND RT ELEVATOR CONTROL CABLE CIRCUITS IAW AMM 27-31-00-750-801-A01. PERFORM ELEVATOR OPS TEST 27-31-00-710-801. PERFORMED OPS TEST OF ELEVATOR IAW AMM 27-31-00-710-801. OPS TESTED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 23,961 hrs · 16,488 cycles

INTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT ASSY ON PANEL 232CZ BROKEN. FOUND SERVICE DOOR EMERGENCY LIGHT IMPROPERLY SECURED. RESECURED LIGHT ASSY BY TIGHTENING SCREW REF AMM 33-51-05-400-801. OPS TESTED GOOD. OK FOR SERVICE.

Part: BRACKET — DISTORTED (LOWER SECTION) · airframe 23,961 hrs · 16,488 cycles

LOWER SECTION GUIDE BRACKETS DISTORTED. R & R ROLLER GUIDE BRACKETS IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 349) · airframe 23,955 hrs · 16,481 cycles

CORROSION AT FS 349 FRAME STRINGER 26L. APPLIED CIC IAW SRM 51-21-11-001-001-A01.

Part: FRAME — DAMAGED · airframe 23,955 hrs · 16,482 cycles

FRAME DAMAGED, REPAIRED IAW REO 670-53-61-816.

Part: FRAME — CORRODED (BS 364) · airframe 23,955 hrs · 16,481 cycles

CORROSION AT FS 364 STRINGER 26 L/R. REPAIRED.

Part: SKIN — CHAFED (RUDDER) · airframe 23,954 hrs · 16,481 cycles

MINOR CHAFING TOP TO BOTTOM ON BOTH SIDES OF RUDDER SKIN FROM RUDDER SEAL RUB. L/E SKINS UPPER & LOWER ON LT & RT SIDES NEED PAINTED. PAINTED BLUE AND LIGHT RED ON LT & RT SIDES OF L/E SKINS AS REQUIRED IAW SRM 51-25-01-001-001-A01. DARK RED REQUIRES TO BE PAINTED ON LT & RT SIDES OF L/E SKIN WHEN RECEIVED. PAINTED DARK RED ON LT & RT SIDES OF L/E SKINS AS REQUIRED IAW SRM 51-25-01-001-001-A01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW ASA SOP 5702. RII FOUND TO BE SATISFACTORY.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 23,955 hrs · 16,481 cycles

LOWER AFT PAX DOOR CORNER CORRODED. REMOVED AND REPLACED LOWER AFT PAX DOOR CORNER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 859-969) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 859 TO 969 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-(A01) FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-(A01). R & R SEAT TRACK IAW AMM 53-00-49-000-801(A02), 53-00-49-400-801(A02).

Part: SEAT TRACK — CORRODED (BS 785.15-859) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 785.15 TO 859 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801(A02) 53-00-49-400-801(A02).

Part: SEAT TRACK — CORRODED (BS 573-669) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 573 TO 669 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R RT SIDE SEAT TRACK IAW AMM 53-00-47-000-801.

Part: SEAT TRACK — CORRODED (BS 839-969) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 839 TO 969 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE WITHIN LIMITS IAW SRM 53-51-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 669-712) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 669 TO 712 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-010-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785.15-859) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 785.15 TO 859 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACK IAW AMMM 53-00-49-000-801-A01 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 712-761.85) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 712 TO 761.85 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACKIAW AMM 53-00-49-000-801(CONGIG A02) AMM 53-00-49-400-801 (CONFIG A02).

Part: RAIL — CORRODED (BS 712-761.85) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 712 TO 761.85 HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-41-49-101-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02, 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 472-573) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 472 TO 573 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED 0.039" FOUND OUT OF LIMITS IAW SRM 53-31-49-101-001-A01, FIG 53-31-49-191-804. R & R SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 669-712) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 669 TO 712 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-001-001-A01, SEAT RAIL FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT RAIL IAW AMM 53-00-49-000-801 (CONFIG A02) AMM 53-00-49-400-801 (CONFIG A02) RB 88122.

Part: SEAT TRACK — CORRODED (BS 573-669) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 573.00 TO 669.00 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801(CONFIG A02) AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 859-969) · airframe 23,955 hrs · 16,481 cycles

SEAT TRACK FROM FS 859 TO 969 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A02) AMM 53-00-49-400-801.

Part: ATTACH ANGLE — CORRODED (CARGO DOOR) · airframe 23,955 hrs · 16,481 cycles

ATTACH ANGLES CORRODED AT TOP END. REMOVED AND REPLACED ANGLES AT TOP END OF ASD IAW SRM 51-42-06-0001-001-A01.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 23,955 hrs · 16,481 cycles

RT EMERGENCY EXIT FAILED FUNCTIONAL CHECK. TOOK 62LBS TO UNLOCK. CLEANED, LUBED AND C/W FUNCTIONAL CHECK IAW AMM 52-21-00-720-801, CHECKED GOOD.

Part: CHANNEL — CORRODED (BS 295-310) · airframe 23,955 hrs · 16,481 cycles

CHANNEL HAS CORROSION BETWEEN FS 295-310 S27 AROUND ANTENNA. CHANNEL FOUND TO BE CORRODED OUT OF LIMITS. REMOVED CHANNEL IAW SRM 51-42-06-001-001. INSTALLED SERVICEABLE CHANNEL IAW SRM 51-42-06-001-001 & 51-42-21-001-001.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 23,955 hrs · 16,481 cycles

FWD EQUIPMENT COMPARTMENT FLOOR CRACKED. REMOVED AND INSTALLED FLOOR PANEL IAW REO 670-53-11-509 REV-.

Part: WEB — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

FS 280 WEB LT SIDE CORRODED. REPAIRED IAW REO 670-53-11-594 01 AND GENERIC REO 670-53-11-594 REV. PERFORMED EDDY CURRENT INSP OF WEB CUTLINE PER REO 670-53-11-594, NOTE IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 23,955 hrs · 16,481 cycles

INTERCOSTAL HAS CORROSION AT FS 364 S26L/R. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 23,955 hrs · 16,481 cycles

FRAME CORRODED AT FS 310, S27R. EVALUATED DAMAGE FOUND TO BE OUT OF LIMITS. PERFORMED NDT INSPECTION IAW NDTM 51-20-006-250-A01, NO INDICATIONS NOTED. DRILLED & DEBURRED NEW FRAME SECTOR REF REO 670-53-21-839. FABRICATED FRAME SPLICE ANGLE, STRINGER CLEATS IAW REO 670-53-21-839. INSTALLED IAW REO 670-53-21-839.

Part: FRAME — CORRODED (BS 349) · airframe 23,955 hrs · 16,481 cycles

FRAME CORRODED AT FS 349 AT S26L. REMOVED CORRODED FRAME SECTOR AND FOUND CORROSION EXCEEDS ALLOWABLE LIMITS IAW SRM 53-21-06-101-006-A01 AND SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-06-001-001. INSTALLED FRAME IAW SRM 51-42-06-001-001-A01.

Part: STRAP — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

FS 280 STRAP CORRODED AT S27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT, IS .079" ORIGINAL IS .080, MATERIAL REMOVED IS .001. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-101-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

ANGLE BRACKET FOR FLOORBOARD CORRODED ON AFT SIDE OF FS 280 AT S27. R & R ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

FLOORBEAM FS 280 FOUND CORRODED. REMOVE AND REPLACED ANGLE IAW SRM 51-42-06-001-001, 51-42-21-001-001, AND 51-421-22-001-001.

Part: FRAME — CORRODED (BS 319) · airframe 23,955 hrs · 16,481 cycles

FRAME CORRODED AT FS 319 S27R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FRAME SPLICE IAW REO 670-53-21-840.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,955 hrs · 16,481 cycles

AFT CARGO DOOR LOWER SILL ANGLE HAS MINOR CORROSION. REMOVED LIGHT CORROSION AT AFT CARGO DOOR LOWER SILL ANGLE IAW SRM 51-21-06-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

FS 280 CROSSBEAM CORRODED. REMOVED AND REPLACED CROSSBEAM IAW SRM 50-42-06-001-001, 51-42-13-001-001, 51-42-22-001-001.

Part: WEB — CORRODED (BS 280) · airframe 23,955 hrs · 16,481 cycles

FS 280 WEB RT SIDE CORRODED. CUT OUT DAMAGE IAW REO 670-53-11-594 01 AND REO 670-53-11-594 REV. PERFORMED EDDY CURRENT INSPECTION OF WEB CUTLINE PER REO 670-53-11-594 IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED.

Part: SAFETY VALVE — FAILED (CABIN ALITITUDE) · airframe 22,758 hrs · 15,656 cycles

CABIN ALTITUDE CAUTION MESSAGE COMPLIED WITH QRH. ECS PAGE ALL GREEN LINES FLASHING. AT 21000 FT IT APPEARED THAT PRESSURATION STARTED WORKING AGAIN. ENROUTE TO SWF ACFT DIVERTED, EMERGENCY DECLARED AS A PRECAUTION. R & R NR1 SAFETY VALVE IAW AMM 21-32-03. OPS CHECKED GOOD. NO FAULTS NOTED AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,630 hrs · 14,893 cycles

EMERGENCY FLOOR FLOOD LIGHT AT 12A/B HAS SEVERAL BULBS INOP. RELAMPED EMERGENCY FLOOR FLOOD LIGHT AT 12 A/B. OPS CK GOOD IAW AMM 33-51-11. RELAMPED EMERGENCY FLOOR FLOOD LIGHT AT 12 A/B. OPS CK GOOD IAW AMM 33-51-11.

Part: LIGHT — MISSING (CABIN) · airframe 21,598 hrs · 14,866 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT MISSING. REPLACED SERVICE DOOR EMERGENCY EXIT FLOOD LIGHT IAW AMM 33-51-11.

Part: SKIN PANEL — CORRODED (BS 985-1108) · airframe 21,478 hrs · 14,774 cycles

CORROSION FOUND ON FUSELAGE SKIN PANEL BETWEEN FS 985-1108 BETWEEN STR 24RT-25LT. (OPEN)

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 21,103 hrs · 14,521 cycles

EXIT PLACARD ON PASSENGER DOOR IS NOT READABLE. REPLACED EXIT PLACARD ON PASS DOOR IAW AMM 11-20-00.

Part: LIGHT — INOPERATIVE (ROW 4) · airframe 19,883 hrs · 13,690 cycles

REFER TO DMIL 565309-2 CEILING EMERGENCY FLOODLIGHT AT ROW 4 INOP. FOUND PUSHED PIN AT FLOODLIGHT ASSY, RESEATED PIN IAW ESPM 20-26-03. OPS CHECK IAW AMM 33-51-00. OPS GOOD DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 19,832 hrs · 13,652 cycles

CEILING EMERGENCY LIGHT AT ROW 4 DOESN`T COME ON. FOUND PUSHED PIN AT FLOODLIGHT ASSY- RESEATED PIN PER ESPM 20-26-03 OPS CHECK IAW AMM 33-51-00. OPS GOOD DEFER CLEARED PLACARD REMOVED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,535 hrs · 13,424 cycles

EXIT EMERGENCY LIGHT JUST AFT OF THE PAX DOOR IS INOP. RELAMPED LT SIDE EXT EMERGENCY LIGHT NR 1 IAW AMM 33-51-15. OPS CK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,378 hrs · 13,302 cycles

MAIN CABIN BOTH EMERGENCY EXIT SIGNS AT RT SIDE CLASS DIVIDER INOP. COMPLIED WITH RIL NR 2029 707 LETTER FOR INSTALLING WIRES FOR EMERGENCY EXIT SIGNS AT RT SIDE CLASS DIVIDER AND PERFORMED SUCCESSFUL OPS TEST OF EMERGENCY LIGHT IAW AMM 33-51-00-710-801-A01 AND 33-51-17-710-A01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 19,347 hrs · 13,276 cycles

MAIN CABIN- SEAT ROW 11 CEILING PANEL, EMERGENCY LIGHT INOP. REINSTALLED LOOSE CONNECTOR AND OPS CHECKED OK IAW AMM 33-51-09.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 19,347 hrs · 13,276 cycles

MAIN CABIN G1 GALLEY- EMERGENCY LIGHT LENS CRACKED. R & R LIGHT LENS ASSY IAW AMM 33-51-05.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,347 hrs · 13,276 cycles

FWD GALLEY AREA FWD F/A PANEL EMERGENCY LIGHT LENS CRACKED. R & R FWD GALLEY AREA FWD F/A PANEL EMERGENCY LIGHT ASSY IAW MM 33-51-05. OPS CHECK GOOD IAW MM 33-51-05.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 19,219 hrs · 13,182 cycles

EMERGENCY LIGHT CABIN CEILING LIGHT 2 (DS142 & 4 (DS144) ARE OFF. TROUBLESHOT & FOUND 1EA PULLED PINS ON THE CONNECTORS FOR EACH EMERGENCY CEILING LIGHT. PUSHED OINS BACK INTO CONNECTORS & RECONNECTED THE CONNECTOR, OPS CHECK GOOD REF MM 35-50-11 & AMM 33-51-00-710-802.

Part: DOUBLER — CORRODED (BS 280) · airframe 19,201 hrs · 13,168 cycles

FS 280 REINFORCEMENT DOUBLERS, 2EA ON LT SIDE AT LBL9.0 AND 1EA ON RT SIDE AT RBL9.0 ARE CORRODED AND REQUIRE REPLACEMENT. (EC) (RESOLVED ON W/O: 155620 TASKCARD: N/R-00417 ) FABRICATED NEW BA670-30069-7 DOUBLER, USING S6144-33 SALVAGE ANGLE P/O T000002550 IAW DWG BA670-30069 REV A. FABRICATED NEW BA670-30069-11 DOUBLER, USING S6144-33 SALVAGE ANGLE P/O T000002550 IAW DWG BA670-30069 REV A. FABRICATED NEW BA670-30069-8 DOUBLER, USING S6144-33 SALVAGE ANGLE P/O T000002550 IAW DWG BA670-30069 REV A. PRIMED AND TOPCOAT APPLIED TO NEW PARTS IAW SRM 51-25-00. FABRICATED NEW BA670-30069-9 DOUBLER FOR LT SIDE, USING S6144-33 SALVAGE ANGLE P/O T000002550 IAW DWG BA670-30069, REV A. INSP REF NDTM 51-20-006. NO DEFECTS IN 4 (EA) FABRICATED DOUBLERS.

Part: STIFFENER — CRACKED (BS 280) · airframe 19,201 hrs · 13,168 cycles

WEB STIFFENER AT FS280, RBL26 CRACKED. CUT AWAY DAMAGED SECTION OF RBL26, FS280 IAW 51-24-36-001-001-A01 (SRM). FABRICATED REPAIR PARTS IAW SRM 51-24-21-001-001-A01 & 51-71-59-001-001-A01. MATERIAL ID 7075 T-6 .032 P/O 110062. 7075 T-6 .040 P/O 107559. ALODINED, PRIMED & PAINTED IAW AMM 51-21-00-380-801-A01 & SRM 51-25-06-001-001-A01 & 51-25-16-001-001-A01. INSTALLED REPAIR SRM 51-71-59-001-001-A01 & 51-42-06-001-001-A01.

Part: FITTING — CORRODED (BS 280) · airframe 19,201 hrs · 13,168 cycles

CLIP AT FS280.00/RBL 11.0 HAS CORROSION. REMOVED CLIP AT FS280 RBL11.0 IAW SRM 51-45-06. 51-42-13. REINSTALLED CLIP AT FS280, RBL11.0 IAW SRM 51-42-13. REMOVED LIGHT SURFACE CORROSION FROM CLIP IAW SRM 51-21-06. TREATED & PRIMED BARE METAL IAW SRM 51-21-11. APPLIED TOP COAT ON CLIP AT FS 280, RBL11.0 IAW SRM 51-29-01-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 19,201 hrs · 13,168 cycles

COCKPIT FLOOR SUPPORT AT FS 280.00 CORRODED. REMOVED FS 280 COCKPIT FLOOR SUPPORT REF SRM 51-42-06-001-001-A01. CORROSION BEYOND LIMITS. DRILLED UP NEAR COCKPIT FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED NEW COCKPIT FLOOR SUPPORT REF SRM 51-42-06-001-001-A01. INSTALLED OTBD LT CAMLOCK REF SRM 51-42-06-001-001.

Part: BEAM — CORRODED (BS 693) · airframe 19,201 hrs · 13,168 cycles

CORROSION FOUND ON BEAM BULKHEAD AT RBL 9 FS 693.00. CORROSION ON RBL9 BULKHEAD BEAM IS OUT OF LIMITS, NO DAMAGE ALLOWED IAW SRM 53-41-10-101-001-AO1. FWD LOCATION DRILLOUT DAMAGE HOLE TO 5/32 & SPOTFACE LOWER AFT LOCATION DILLOUT DAMAGE HOLE TO 5/32 & SPOTFACE HOLE. REMOVE FWD & AFT SPLICE (6) NUTPLATE. REF REO 670-53-41-097 REV-- DATE 2010-04-24. REPAIR ITEM 1, 2, 3. C/W REO 670-53-41-097 REV A DATED 4-30-10. REVERSED SPOTFACE HOLE LOCATION 3, REF REO 690-53-41-097 REV A DATED 2010-04-30. C/W ASA ECTC REO 670-53-41-097. C/W ASA RII PER ECTC REO 670-53-41-097.

Part: FLOOR SUPPORT — CORRODED (BS 469-510) · airframe 19,201 hrs · 13,168 cycles

CORROSION FOUND ON RT FLOORBEAM AT RBL 9.0 BETWEEN FS469.00 - 510.00. REMOVED CORROSION REF, SRM 53-31-43-101-001-AO1 & FOUND OUT OF LIMITS, UT THICKNESS TEST REF NDTM 51-20-004. MIN THICKNESS READING READ .031" IN BLENDED AREA. CUT OUT FLOORBOARD SECTION IAW SRM 51-24-36-001-001-AO1. NDT RT FLOORBEAM CUT LINE IAW NDTM 51-20-06. NO DEFECTS NOTED. FABRICATED REPAIR PARTS. TRIMMED NEW FLOORBOARD SECTION IAW SRM 51-24-36-001-001-AO1. INSTALLED NEW FLOORBEAM. INSTALLED REPAIR PARTS, ET INSPECTION REF NDTM 51-20-006. NO DEFECTS NOTED IN FABRICATED PARTS. INSTALLED CLEATS IAW PRELIMINARY REO 670-53-00-254. DATED 5-7-10. INSTALLED SHIMS & SPLICE ANGLES IAW PRELIMINARY REO 670-53-00-254 DATED 5-7-10.

Part: FLOOR SUPPORT — CORRODED (BS 581) · airframe 19,201 hrs · 13,168 cycles

CORROSION FOUND ON RT LONGITUDINAL FLOOR SUPPORT IS OUT OF LIMITS AT FS 581.00. PERFORMED CUTOUT OF DAMAGED SECTION OF FLOOR SUPPORT IAW SRM 53-00-41. LOCATED NEW PIECE OF FLOOR SUPPORT IAW SRM REPAIR SRM 53-00-41-991-830. FABRICATED 1EA AFT LOWER SPLICE REF SRM 53-00-41. FABRICATED, LOCATED AND DRILLED 2 CLEATS, 1 SHIM AND 1 LOWER SPLICE IAW SRM 53-00-41. ET INSP REF NDTM 51-20-006, NO DEFECTS NOTED. INSTALLED NEW PIECE OF FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. LOCATED AND INSTALLED IAW PRELIMINARY REO 670-53-00-254. REF ITEM 11.

Part: FLOOR SUPPORT — CORRODED (BS 581-684) · airframe 19,201 hrs · 13,168 cycles

CORROSION FOUND ON RT LONGITUDINAL FLOORBEAM AT RBL9.0 BETWEEN FS581.00 & 684.00. CORROSION ON FLOORBEAM AT RBL9 BETWEEN FS581.00 & 684.00. REMOVED IAW SRM 51-21-06. UT THICKNESS TEST REF NDTM 51-20-004. THICKNESS READINGS RANGED .059-.124" IN BLEND. DAMAGE AT FS581.00 OUT OF LIMITS IAW SRM 53-31-43-101-001-A01. SPLICE REPAIR DUE; TRANSFERED WORK 7105725/76. DAMAGE AT FS684.00 WITHIN LIMITS IAW SRM 53-31-43-101-001-A01. RESTORED FINISH IAW A023 OD SRM 51-21-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 19,201 hrs · 13,168 cycles

RT CABIN SIDEWALL SEAT TRACK FROM FS573-675 HAS CORROSION. REMOVED CORROSION FROM SEAT TRACKS AT FS573-672 RT IAW REO 670-53-00-013 REV B. ALODINED SEAT TRACKS IAW SRM 51-21-16.

Part: STRINGER — CRACKED (BS 280 S3L) · airframe 19,201 hrs · 13,168 cycles

AT FS280 THE FWD END OF STR 3L IS CRACKED (LINTEL). CUTOUT DAMAGE IAW NOTE 1 OF REO 670-53-21-493, REV A DATED 2-17-10. NDT FS280 LINTEL IAW NDTM 51-20-06. NO DEFECTS NOTED. INSTALLED REPAIR PARTS IAW REO 670-53-21-493, REV A DATED 2-17-10. LEAK CHECK GOOD LINTEL AMM 21-50-00-862-801. CC21 5-9-10. (12) 8.

Part: FLOORBEAM — CRACKED (FS 280.00) · airframe 19,201 hrs · 13,168 cycles

FLOORBEAM CRACKED AT FS 280.00. INSTALLED NEW FS280 FLOORBEAM IAW SRM 51-23-00-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-42-13-001-001-A01 & REO 670-53-11-047, REV E 08/13/09.

Part: FRAME — CORRODED (BS 517 S9L) · airframe 19,201 hrs · 13,168 cycles

FRAME AT FS 517.00, STR19L IS SEVERELY CORRODED AROUND LIGHTNING HOLE. INSTALLED NEW BRACKET AT FS 517.00 STR 19L REF SRM 51-42-06 AND 51-42-21. LEAK CHECK "GOOD" ON STUB FRAME IAW AMM 21-50-00-86-2-801.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 19,201 hrs · 13,168 cycles

LEFT CABIN SIDEWALL SEAT TRACK HAS CORROSION AT FS 573-675. REMOVED CORROSION FROM SEAT TRACK AT LT FS675-573 IAW REO 670-53-00-013, REV B, ALODINED SEAT TRACKS IAW SRM 51-21-16.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 19,201 hrs · 13,168 cycles

CREW ESCAPE HATCH MISSING (ALL) EXTERIOR PLACARDS. REPLACED ALL EXTERIOR PLACARDS ON CREW ESCAPE HATCH IAW AMM 26-60-04.

Part: SEAT TRACK — CORRODED (BS 485-969) · airframe 19,201 hrs · 13,168 cycles

RT FLOOR SEAT RAILS AT RBL 9 FROM FS 485-969 HAVE CORROSION. SEAT RAIL FOUND OUT OF LIMITS IAW SRM 53-31-49. REMOVED SEAT RAILS IAW AMM 53-00-49-000-801. REPLACED SEAT RAIL IAW SRM 51-41-02 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 374-484) · airframe 19,201 hrs · 13,168 cycles

LEFT CABIN SEAT TRACK AT LBL9.0, FS374-484 CORRODED BEYOND LIMITS. REMOVED LT CABIN SEAT RAIL SECTION AT FS374-485 LBL9.0 USING NR 2 PHILLIP HEAD SCREW DRIVER AMM 53-00-49-000-801-A02. INSTALLED NEW FABRICATED SEAT RAIL AT FS 374-485 LBL 9.0 AMM 53-00-49-400-801-A02. FABRICATED NEW SEAT RAIL PN SH670-32249-3 FROM N126-2075 SEAT TRACK EXTRUSION P/O T-2509 SRM 51-41-02. APPLIED ALODINE TO SEAT RAIL SRM 51-21-10 DATE A044.

Part: SEAT TRACK — CORRODED (BS 349-573) · airframe 19,201 hrs · 13,168 cycles

RIGHT CABIN SEAT TRACK FROM FS349-573 HAVE CORROSION (SIDEWALL TRACKS). FOUND OUT OF LIMITS IAW SRM 53-21-51. REPLACEMENT NOT REQUIRED, PERFORMED REO 670-53-00-013. PERFORMED BLEND REPAIR IAW REO 670-53-00-013, REV B, DATE 2009-06-18. ALODINED SEAT TRACKS AS SRM 51-21-16

Part: SEAT TRACK — CORRODED (BS 349-484) · airframe 19,201 hrs · 13,168 cycles

RIGHT CABIN SEAT TRACK AT RBL9.0, FS349-484 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT RBL 9 FROM FS 349-484 AS IAW SRM 51-41-02. INSTALLED NEW SEAT TRACK AT RBL 9 FROM FS 349-FS 484, REF AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-573) · airframe 19,201 hrs · 13,168 cycles

LEFT SIDE CABIN SEAT TRACKS FROM FS349-573 HAVE CORROSION (SIDEWALL TRACKS). SEAT TRACK CORRODED BEYOND LIMITS, REPLACEMENT NOT REQUIRED, REPAIRED IAW REO 670-53-00-013, REV B, DATE 2009-06-18. REMOVED CORROSION FROM SEAT TRACK FS349-573 LT IAW REO 670-53-00-013 REV "B" DATE 2009-06-18. ALODINED SEAT TRACKS IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 675-761) · airframe 19,201 hrs · 13,168 cycles

LT SIDE SEAT RAILS FROM FS675-761 HAVE CORROSION. CORROSION BEYOND LIMITS, REPLACEMENT NOT REQUIRED REPAIR IAW REO 670-53-00-013, REV B, DATE 2009-06-18. BLENDED OUT LT SIDE SEAT RAILS FROM FS675-761 REF REO 670-53-00-013, REV B DATE 2009-06-18. APPLIED ALODINE IAW SRM 51-21-16.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,201 hrs · 13,168 cycles

CROSSBEAM AT FS 280.00 CORRODED FROM LBL 27.00 TO RBL 27.00. WORK ACCOMPLISHED ON JOB 7105725.

Part: SEAT TRACK — CORRODED (BS 485-969) · airframe 19,201 hrs · 13,168 cycles

LEFT FLOOR SEAT RAILS AT RBL 9 FROM FS 485-969 HAVE CORROSION. SEAT RAILS CORRODED BEYOND LIMITS, REMOVED LT FLOOR SEAT RAILS REF AMM 53-00-49-000-801 PARAGRAPH 4C. INSTALLED LT SEAT RAILS IAW AMM 53-00-49-400-801(A01). LOCATED & DRILL OUT HOLES IN SEAT TRACK PN N126-2075 P/O T000002509 AT FS836.5 TO 988 LBL9, SRM 51-41-02. FINISHED ALL CUTOUTS & TRIMMING REQUIRED & ALODINED SEAT TRACK IAW SRM 51-20-00.

Part: SEAT TRACK — CORRODED (BS 675-761) · airframe 19,201 hrs · 13,168 cycles

RT SIDE SEAT RAILS FROM FS 675-761 HAVE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-41-51. REPLACEMENT NOT REQUIRED REPAIR IAW REO 670-53-00-013, REV B, DATE 2009-06-18. BLENDED OUT RT SIDE SEAT RAILS FROM FS675-761 REF REO 670-53-00-013 REV B DATE 2009-06-18. APPLIED ALODINE IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 785-969) · airframe 19,201 hrs · 13,168 cycles

LT SIDE SEAT RAILS FROM FS 785-969 HAVE CORROSION. LT CABIN SIDE SEAT RAILS FROM FS785-969 ARE CORRODED BEYOND LIMITS, REPLACEMENT NOT REQUIRED REPAIR IAW REO 670-53-00-013, REV B, DATE 2009-06-18. BLENDED OUT CORROSION ON LT SIDE SEAT RAIL FROM FS 785-969 REF REO 670-53-00-013, REV B, DATE 2009-06-18. APPLIED ALODINED IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 785-969) · airframe 19,201 hrs · 13,168 cycles

RT SIDE SEAT RAILS FROM FS785-969 HAVE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-41-51. REPLACEMENT NOT REQUIRED REPAIR IAW REO 670-53-00-013, REV B, DATE 2009-06-18. BLENDED OUT CORROSION ON RT SIDE SEAT RAIL FROM 785-969 REF REO 670-53-00-013 REV B DATE 2009-06-18. APPLIED ALODINE IAW SRM 51-21-16.

Part: GLOWSTRIP — NONE (CABIN) · airframe 19,201 hrs · 13,168 cycles

SERVICE DOOR ENTRY CLOSE OUT PANEL 232AZ PHOTOLUMINESCENT TAPE IS MISSING FROM LOWER EDGE. REMOVED TAPE FROM 232AZ AT BOTTOM OF PANEL AFTER REMOVAL, FOUND SUSPECTED PHOTOLUMINESCENT STRIP TO BE INSTALLED. NO FURTHER ACTION REQUIRED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,836 hrs · 12,902 cycles

LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LH AFT MOST EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15, OP'S CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,848 hrs · 12,170 cycles

2ND FROM FRONT CABIN CEILING EMERGENCY LIGHT INOP

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,848 hrs · 12,170 cycles

RT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 17,026 hrs · 11,543 cycles

CAPTS FLASHLIGHT BROKEN.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 16,328 hrs · 11,019 cycles

MEGAPHONE INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,237 hrs · 10,956 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 3 INOP.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 16,201 hrs · 10,927 cycles

PAX DOOR WON'T CLOSE.

Part: WARNING SYSTEM — ACTIVATED (SLAT SYSTEM) · airframe 15,390 hrs · 10,322 cycles

SLATS FAIL CAUTION ON FLAPS 8 DEG SELECTION. SLATS 0 DEG, FLAPS 45 DEG. EMERGENCY DECLARED.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 1,425,740 hrs · 9,483 cycles

POSSIBLE CRACK AT LBL 27 UNDER LT SIDE COCKPIT ATTACHES TO FLOOR AND FRAME 280 STRUCTURE AREA IS MARKED. REPAIRED COCKPIT FLOOR INTERCOSTAL AT FS 280 AND LBL 33.0 IAW REO 670-53-11-304. REFER TO ATTACHED M-234 FOR WORK PERFORMED. EC/TC REO 670-53-11-304 COMPLIED WITH. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (BS 669 S15R) · airframe 1,425,740 hrs · 9,483 cycles

CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT STR 15R FS 669.00 TO FS 977.00-(MARKED). BLENDED CORROSION FOUND ON SIDE SEAT RAIL AT STR 15R FS 669 TO FS 977 REMOVED .014" OF MATERIAL WITHIN LIMITS OF CRJ 700 SRM 53-41-49 AND 53-51-49. RESTORED SURFACE FINISH AND RE-IDENTIFIED SEAT RAILS AS PER CRJ 700 SRM 53-41-49 AND 53-51-49. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 6/24/08.

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 349.00 TO FS 477.40. BLENDED DAMAGE ON ON CABIN FLOOR SEAT TRACKS FS 349 TO FS 477 REMOVED .015" OF MATERIAL. WITHIN LIMITS ALLOWED .035" WORK DONE IAW SRM 53-21-49.

Part: WEB — CORRODED (BS 280) · airframe 1,425,740 hrs · 9,483 cycles

LT 280 WED CORRODED---[OPEN] (B)

Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL9 FS 379.00 TO FS 477.40. BLENDED CORROSION ON LBL 9 FS 349 TO FS 477.40 REMOVED .020" OF DAMAGE WITHIN LIMITS ALLOWED .035" OF REMOVAL. ALL WORK DONE IAW SRM 53-21-49. DK 7022603 JOB COMPLETE.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 1,425,740 hrs · 9,483 cycles

CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15L FS 379.00 TO FS 669.40. BLENDED DAMAGE FOUND ON S15L FS 379 TO FS 669.40 REMOVED .024" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035". ALL WORK DONE IAW SRM 53-21-49 AND 53-31-49.

Part: SEAT TRACK — CORRODED (BS 477-693) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL 9 FS 477.40 TO FS 693.00. BLENDED CORROSION ON CABIN FLOR SEAT RAILS LBL 9 FS 477 TO FS 693 REMOVED .021" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-31-49.

Part: SEAT TRACK — CORRODED (BS 693-977) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL 9 FS 693.00 TO FS 977.00. BLENDED CORROSION FOUND ON LBL 9 FS 693 TO FS 977 REMOVED .028" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-41-49 AND 53-51-49.

Part: WEB — CORRODED (BS 280) · airframe 1,425,740 hrs · 9,483 cycles

RT 280 WEB CORRODED. OPEN (B)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 1,425,740 hrs · 9,483 cycles

280 SUPPORT BEAM CORRODED. REMOVED AND REPLACED STA 280 SUPPORT BEAM PN CC670-34175-7 AS PER SRM 51-42-21, 51-42-06. REO 670-53-11-047, AND SB 670BA-53-026.

Part: SEAT TRACK — CORRODED (BS 669-977) · airframe 1,425,740 hrs · 9,483 cycles

CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15L FS 669.00 TO FS 977.00. BLENDED CORROSION FOUND ON S15L FS 669.00 TO FS 977.00 REMOVED .019" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-42-49 AND 53-51-49.

Part: SEAT TRACK — CORRODED (BS 693-677) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 693.00 TO FS 977.00. BLENDED CORROSION FOUND ON RBL 9 FS 693 TO FS 977 REMOVED .018" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-41-49 AND 53-51-49.

Part: SEAT TRACK — CORRODED (BS 477-693) · airframe 1,425,740 hrs · 9,483 cycles

CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 477.40 TO FS 693.00. BLENDED CORROSION FOUND ON RBL 9 FS 477.40 TO FS 693.00 REMOVED .005" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" ALL WORK DONE IAW SRM 53-31-49.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 1,425,740 hrs · 9,483 cycles

CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15R FS 379.00 TO FS 669.40. BLENDED CORROSION FOUND ON S15R FS 379 TO FS 669.40 REMOVED .015" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-31-49.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 1,425,740 hrs · 9,483 cycles

VERTICAL STAB LOWER RT DRAG ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT V/STAB TO FUSELAGE DRAG ANGLE TO LOCATE END OF CRACK IAW NDTM 51-20-006 END OF CRACK IS MARKED. CUT AWAY DAMAGE FROM VERTICAL STAB LOWER RT DRAG ANGLE IAW REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES ON RIGHT VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW REO 670-55-31-018 PER NDTM 51-20-006 NO DEFECTS NOTED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

VERTICAL STAB LOWER LT DRAG ANGLE IS CRACKED CUT AWAY DAMAGE FROM VERTICAL STAB LOWER LT DRAG ANGLE IAW REO 670-53-31-018. INSTALLED DOBLER AND FILLER, FILLET SEAL REPAIR PARTS AND FINAL PAINT AND LT DRAG ANGLE. ALL WORK DONE IAW REO 670-53-31-018. (B)

Part: PLACARD — WORN (PAX DOOR) · airframe 1,425,740 hrs · 9,483 cycles

PAX DOOR EXIT PLACARD WORN. REPLACED EXIT PLACARD PER AMM 11-30-02.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 12,324 hrs · 8,126 cycles

AFT CARGO DOOR INDICATES OPEN IN FLIGHT. AFT CARGO DOOR AMBER CAUTION MSG ILLUMINATED. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,207 hrs · 8,046 cycles

F/A FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,956 hrs · 7,872 cycles

AFT MOST CEILING EMERGENCY LIGHT INOP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,213 hrs · 7,375 cycles

FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REMOVED FS 280 FWD CENTER FLOOR SUPPORT ANGLE MH715 LOCATED HOLES IN SERVICEABLE ANGLE P/N CC670-33292-13 IAW CRJ SRM 51-40-11 MH715. OK TO INSTALL. INSTALLED FWD CENTER FLOOR SUPPORT IAW CRJ CRM 51-42-06 & 51-42-21 JA10220 2-27-07. OK TO TOPCOAT. TOPCOATED IAW CRJ SRM 51-25-16 JA10220 2-27-07. REINSTALLED AVIONICS COMPARTMENT LIGHT TO FS 280 SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06. MDA1064 2-27-07. SUPPLEMENTAL - SDR CLOSED 03/01/07.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,213 hrs · 7,375 cycles

LEFT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED LT LOWER FS 280 WEB. REF STEPS OF FORM 412 FOR DUPLICATION OF WEB. OK TO INSTALL STRAP TO DOUBLER. INSTALLED 2 EA. LOWER ROWS OF FASTENERS W/ WET SOLID FASTENERS IAW CRJ SRM 51-42-6 MH715. OK TO INSTALL LT 280 WEB. INSTALLED LT 280 WEB IAW CRJ 7001900 SRM 51-42-06, 51-42-13, 51-42-21. TOPCOATED INTERIOR WALL / GRAY WITH AXWF-3-G3G IAW CRJ 700/900 SRM 51-25-00 WR586 2-26-07. APPLIED WHITE TOPCOAT TO REMAINING FASTENERS IAW CRJ 700/900 SRM 51-25-16. WR586 2-26-07.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,213 hrs · 7,375 cycles

RT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED RT 280.00 WEB. DUPLICATED WEB 0.040 7075T-6. LOCATE ALL HOLES EXCEPTING THOSE FROM RBL 42.50 OUTBOARD. DEBURR ALL ALODINE, PRIME TOPCOAT, IAW REO 670-53-11-052. DUPLICATED STRAP RT. STRAP ATTACHED TO WEB, IAW REO 670-53-11-052. REMOVED STRAP FROM WEB TO ACCOMMODATE REO 670-53-11-201 REPAIR. OK TO INSTALL WEB ASSY ON RT 280. INSTALLED A LARGE PORTION OF RT 280 WEB, IAW REO 670-53-11-052. INSTALLED REQUIRED FASTENERS IN RT 280 WEB, IAW REO 670-53-11-052. ALL FASTENERS INSTALLED IN RT 280.00 WEB, IAW REO 670-53-11-052. OK TO PRIME / TOPCOAT PRIMED / TOPCOATED WEB FASTENERS, IAW CRJ 700/900 SRM 51-25-06, 51-25-16 AND 51-25

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,213 hrs · 7,375 cycles

FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REPLACE BEAM PER CUSTOMER. REMOVED ALL REQUIRED FASTENERS ON LEFT FS 280. CROSSBEAM, REMOVED LBL 9 CLIP, REMOVED LEFT FS 280 CROSSBEAM. ALL WORK DONE IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21. LOCATED HOLES ON SERVICEABLE BEAM P/N CC670-34175-7 IAW CRJ SRM 51-40-11 MH715. OK TO INSTALL LEFT 280 CROSSBEAM. OK TO INSTALL LBL 9 CLIP. INSTALLED LBL 9 WITH HI-LOKS, INSTALLED LEFT FS 280 CROSSBEAM WET W/ HI-LOKS, SOLID FASTENERS, CHERRY RIVETS IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21 MH715, REQUIRES 1 EA. CHERRY FASTENERS 2ND IN FROM O/B REQUIRES CHANGING. REMOVED CHERRY FASTENER 2ND IN FROM O/B REQUIRES CHANGING. REMOVED CHERRY FASTENER & INSTALLED HI-LOK IAW

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,213 hrs · 7,375 cycles

PAX DOOR OUTER HANDLE APPEARS TO BE CRACKED AT INNER AFT RADIUS (MARKED) REF: 52-830-102 PG 7, FIG 52-11-02 ATTACHED. PERFORMED LPI ON PANEL DOOR OUTER HANDLE INNER RADIUS VERIFIED CRACK IS PRESENT. IAW CRJ 700 NDT MANUAL 51-20-00-08. REPAIRED PER APPLICABLE MATERIALS. PERFORMED OPS CHECK IAW CRJ 700 AMM 52-11-03. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,213 hrs · 7,375 cycles

DURING PREFLIGHT INSPECTION, FOUND EXTERIOR EMERGENCY LIGHTS INOP/CREW RESET CB, NO HELP.

Part: STEP — BROKEN (AIRSTAIR) · airframe 10,103 hrs · 6,645 cycles

ASD BOTTOM STEP BROKEN AT ATTACH LINK.

Part: LAMP — BURNED OUT (EMERGENCY LGIHT)

DURING AN A-CHECK, THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4413 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN OKC, THE STRUT ON THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND THE CONNECTING ROD SUPPORT ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LENS — CRACKED (CABIN)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. (ASOA04337)

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR.

Part: STEP — CRACKED (PAX DOOR) · airframe 3,930 hrs

DURING C-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: CONTROL UNIT — MALFUNCTIONED (ELEVATOR)

DURING CLIMB-OUT FROM OAK-DFW, THE CREW RECEIVED A SPLIT ELEVATOR CAUTION LIGHT. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES REQUESTED FOR STAND BY AS A PRECAUTION. THE AIRCRAFT RETURNED TO OAK AND LANDED SAFELY. MAINTENANCE RESET THE ELEVATOR CONTROL SYSTEM AND PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE)

DURING CLIMB-OUT FROM ATL-AGS, THE CREW RECEIVED A RIGHT BLEED DUCT WARNING MESSAGE. QRH WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE READJUSTED THE LOOP ELEMENTS AT MT143 AND 144 AND MT204 AND 205 WHICH WERE FOUND TO BE TOUCHING THE DUCTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — STUCK (FUSELAGE)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND TO BE STUCK CLOSED. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES BUT COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)