N858AS

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 34,886 hrs · 31,561 cycles

EXIT LIGHT ON F/A STATION INOPERATIVE. R & R WIRE SPLICE CONNECTOR ON EMERGENCY LIGHT, DS10LN, IAW ESPM 20-17-31. OPS TEST GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 34,875 hrs · 31,545 cycles

EXIT LIGHT TRIM PANEL NEXT TO GALLEY 1 HAS A BROKEN WIRE. TERMINATED FEMALE SPLICE CONNECTOR FOR EXIT LIGHT ON RT FWD DOOR TRIM IAW ESPM 20-17-31. PERFORMED OPS TEST OF EXIT LIGHT IAW AMM 33-51-00, EXIT LIGHT PASSED, OPS TEST.

Part: FLOOR SUPPORT — CORRODED (BS 554-559) · airframe 34,875 hrs · 31,545 cycles

FLOORBEAM CAP CORRODED BETWEEN FS 554.00 +64 AND FS 559.0+45 AT RBL9. REMOVED CORROSION FROM FLOORBEAM AT RBL 9 BETWEEN FS 559.00+48-559.00+64 IAW SRM 51-21-06. REPAIR OR REPLACE BLEND AREA OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH SRM FLOOR SUPPORT STRUCTURE REPAIR NO 1 53-00-43.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 34,875 hrs · 31,545 cycles

FLOORBEAM CORRODED AT FS 621.00, RBL9. REMOVED CORROSION FROM FLOORBEAM AT FS621 AT RBL9 IAW SRM 51-21-06. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43 AND SRM 53-00-00. DRILLED NEW SERIVCABLE FLOORBEAM AT RBL9, FS 559+112 TO FS 621 IAW SRM 51-40-11. STARTED INSTALLING FLOORBEAM AT RBL9, FS 559+112 TO FS621 IAW SRM 51-42-21. FINISHED FLOORBEAM INSTALLTION IAW DWG 601R-35031 AND COMPLIED WITH ECTC REO 601R-53-61-3780 AND REO 601R-53-61-3780, REV A DATED 07/15/2011 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,875 hrs · 31,545 cycles

LBL 9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN BS 364 - 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,875 hrs · 31,545 cycles

LBL9 SEAT TRACK CORRODED AND OUT-OF-LIMITS AT FS 394 TO FS 409 + 112. REMOVED SEAT RAIL AT FS 394 - FS 409+112 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL AT FS 394-FS406+112 LBL9 IAW AMM 53-01-11-400-802. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,875 hrs · 31,545 cycles

RBL9, SEAT TRACK CORRODED AND OUT-OF-LIMITS BETWEEN FS 364 TO 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,875 hrs · 31,545 cycles

RBL9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN FS 409 +112 AND FS 394. REMOVED CORRODED SEAT TRACK AT RBL9, FS 394-FS 409+112 IAW TASK 53-01-11-000-802. DRILLED & COUNTERSUNK REQUIRED HOLES IAW SRM 51-40-11 HOLES ALODINED IAW SRM 51-21-11. INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 34,875 hrs · 31,545 cycles

CORROSION ON RBL 9 FLOORBEAM CAP FWD OF FS 409.00 + 16. REMOVED CORROSION ON RBL9 FLOORBEAM CAP FWD PF FS 409.00+16 IAW SRM 51-21-06. REPAIRED IAW SRM 53-00-43. FLOOR SUPPORT STRUCTURE REPAIR NR 2.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 34,875 hrs · 31,545 cycles

BAY DOOR INTERCOSTAL AT BS 349-409 BETWEEN STR 26 AND 27L IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. INTERCOSTAL AT FS 394-FS 409 BETWEEN STR 27-26L IS OUT OF LIMITS IAW SRM 51-21-06. REMOVED IAW SRM 51-42-06. INSTALLED INTERCOSTAL AT FS 394-FS 409 BETWEEN STR 27-26L IAW SRM 51-42-21, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,875 hrs · 31,545 cycles

RIGHT SIDEWALL SEAT TRACK FS364-409.16 HAS CORROSION. REMOVED CORROISON ON RT SIDE SEAT RAIL BETWEEN FS364-409+16 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SIDE SEAT TRACK IAW AMM 53-01-11-000-802, FABRCATED NEW SIDE SEAT RAIL IAW ECTC GREO SERIVCABLE SIDE SEAT TRACK IAW ECTC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,875 hrs · 31,545 cycles

RIGHT SIDEWALL SEAT TRACK FS409+16-409+112 HAS CORROSION. REMOVED CORROSION ON RT SIDE SEAT RAIL BETWEEN FS 409+16-409+112 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED RT SEAT RAIL AT FS409+16-409+112 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL IAW AMM 53-01-11-400-802. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485 REV A.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 34,875 hrs · 31,545 cycles

BS 193 ELECTIRCAL BAY FLOOR CRACKED RT SIDE. REPAIRED ELECTRICAL BAY FLOOR AT BS 193.0, RT SIDE, IAW GREO 601R-53-11-111. UPON FURTHER EVALUATION FOUND GREO 601R-53-11-111 TO NOT BE APPLICABLE TO RT SIDE FS 193 ELECTRICAL BAY FLOOR CRACK REPAIR CANCELED ECTC REO 601R 53-11-111 VIA EMAIL REQUEST. COMPLIED WITH ALL STEPS OF REO 601R-53-11-2843, REV B AND EC/TC REO 601R-53-11-2843.

Part: SKIN — CRACKED (BS 235) · airframe 34,875 hrs · 31,545 cycles

FUSELAGE SKIN IS CRACKED AT FS 235.00 S26R. RECIEVED AND COMPLIED WITH REO 601R-53-11-2844. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV C.

Part: HANDLE — FOULED (SERVICE DOOR) · airframe 34,756 hrs · 31,411 cycles

F/A REPORT MAIN AIR SERVICE DOOR IS HARD TO OPEN. FOUND FOD AT MAIN PAX DOOR LEVEL HANDLE. REMOVED FOD. OPS CHECK TEST GOOD, REF AMM 52-11-21.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 34,685 hrs · 31,338 cycles

RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R INVERTER NR 3 IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,622 hrs · 31,277 cycles

EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD.

Part: FITTING — DAMAGED (HORIZONTAL STAB) · airframe 34,596 hrs · 31,252 cycles

UPPER ATTACH FITTINGS HAD TOOL DAMAGE ON BOTH INBD FACES. BLENDED IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS IAW SRM 55-11-27. REPAIRED IAW REO 601R-55-11-522. CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 33,385 hrs · 30,019 cycles

CEILING EXIT SIGN MISSING. INSTALLED CEILING EXIT SIGN IAW AMM 33-51-14.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 32,167 hrs · 28,798 cycles

FWD CABIN ENTRANCE EMERGENCY FLOOR FLOOD LIGHT COVER MISSING. INSTALLED LENS IAW AMM 33-51-19. OP'S CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,957 hrs · 28,596 cycles

RT EXTERIOR NR 6 EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS TEST OF EXTERIOR EMERGENGY LIGHTS, REPLACED THE BULBS AS REQUIRED IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: SKIN — DAMAGED · airframe 31,385 hrs · 28,043 cycles

A HOLE IS IN THE SKIN OF THE AC RT SIDE AT THE FWD END OF THE FLAP STUB FAIRING THIS WAS FOUND WHILE GIVING AN OK TO INSTALL THE RT FLAP STABILIZER FAIRING. COMPLIED WITH REO 601R-53-41-610. COMPLIED WITH EC/TC REO 601R-53-41-610 IAW REO 601R-53-41-601.

Part: WINDOW FRAME — CRACKED (WINDSHIELD) · airframe 31,385 hrs · 28,043 cycles

WINDSHIELD CENTER POST LOWER RT FITTING CRACKED. REMOVED FITTING ON W/S CENTER POST LWR RT SIDE IAW SRM 51-42-21. DRILLED UP NEW FITTING IAW SRM 51-40-11. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. INSTALLED FITTING IAW SRM 51-42-21 AND DWG 601E-33007.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,385 hrs · 28,043 cycles

UPPER LT FLOOR SUPPORT FITTING CORRODED. LOCATED & DRILLED NEW UPPER LT FLOOR SUPPORT FITTING IAW DWG 601RR38672-7 & SRM 51-42-06. INSTALLED NEW SERVICEABLE FITTING IAW DWG 601R38672 & SRM 51-42-06.

Part: STRAP — CRACKED (LT WING) · airframe 31,384 hrs · 28,042 cycles

LEFT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED STRAP IAW SRM 51-42-20-00 AND SRM 51-42-06-00. INSTALLED IAW SRM 51-42-06, 51-42-20 DWG 601R-10336, REV-H.

Part: FRAME — CORRODED (BS 333) · airframe 31,384 hrs · 28,042 cycles

FRAME BS 333 CORRODED BETWEEN S26 - 27L. REMOVED CORROSION IAW SRM 51-21-06 AND 51-12-00. COMPLIED WITH PERMANENT REPAIR EA 12-2014-046 NDTM PT-1, 51-20-06.

Part: BULKHEAD — GOUGED · airframe 31,384 hrs · 28,042 cycles

SCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE AT RBL 36.20 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH REO 601R-53-61-2155.

Part: BULKHEAD — GOUGED · airframe 31,384 hrs · 28,042 cycles

SCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 27.50 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH REO 601R-53-61-2155.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,384 hrs · 28,042 cycles

PASSENGER DOOR HINGE FUSELAGE SIDE 15TH LUG FROM FRONT IS GOUGED. COMPLIED WITH REO 601R-53-21-814, REV. MAJOR REPAIR.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 31,384 hrs · 28,042 cycles

FLOOR PANEL 282HRF HAS DAMAGED SCREW INSERTS. REMOVED AND INSTALLED NEW INSERTS IAW C AND D RPM 25-6000-1.

Part: FLOOR SUPPORT — CORRODED (BS 439-516) · airframe 31,384 hrs · 28,042 cycles

RIGHT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439 - 516. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: BULKHEAD — GOUGED · airframe 31,384 hrs · 28,042 cycles

SCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 18.00 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. COMPLIED WITH REO 601R-53-61-2155.

Part: PANEL — DAMAGED (STAB) · airframe 31,384 hrs · 28,042 cycles

STAB TIP PANEL 343AR ERODED. REPAIRED ERODED TIP ON TAB PANEL 343AR IAW SRM 51-15-52 AND SRM 51-74-02. REPAIRED LIGHTING PROTECTION STRIP IAW D/G DOCUMENT 7101569,

Part: FLOOR SUPPORT — CORRODED (BS 439-544) · airframe 31,384 hrs · 28,042 cycles

LEFT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439-544. COMPLIED WITH ECTC REO 601R-53-41-666.

Part: BULKHEAD — GOUGED · airframe 31,384 hrs · 28,042 cycles

SCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE BETWEEN LBL 18.00 & LBL 27.50 JUST ABOVE WL 73.50. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH STEP 2 OF REO 601R-53-61-2155.

Part: FRAME — CORRODED (BS 349) · airframe 31,384 hrs · 28,042 cycles

FRAME BS 349 CORRODED BETWEEN S25L AND 26R. R & R FRAME SECTOR IAW SRM 51-42-06-00, 51-42-21-00 AND DWG 601R32005. MAJOR REPAIR.

Part: LUG — GOUGED (DOOR HINGE) · airframe 31,378 hrs · 28,035 cycles

PAX DOOR HINGE LUG 2, 5, 8, 14, 19 & 25 GOUGED. COMPLIED WITH REO 601R-52-11-1347. COMPLIED WITH ECTC REP 601R-52-11-1347. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 625) · airframe 31,378 hrs · 28,035 cycles

LT FS 625 ANGLE BROKEN ON T/E. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21, DWG 601R350126 AND 601-35012.

Part: ATTACH ANGLE — CRACKED (BS 625 BULKHEAD) · airframe 31,378 hrs · 28,035 cycles

AFT BULKHEAD ZEE MEMBER TO SKIN ATTACH ANGLE APPEARS CRACKED. REMOVED ATTACH ANGLE AT FS 625 & STR16L IAW SRM 51-42-06 & SRM 51-42-21. REMOVED & DRILLED UP NEW ATTACH ANGLE REF SRM 51-40-11. INSTALLED ATTACH ANGLE REF SRM 51-42-06 & SRM 51-42-21 & DWG 601R350121.

Part: FLOOR SUPPORT — CRACKED · airframe 31,378 hrs · 28,035 cycles

COCKPIT FLOOR SUPPORT AFT LT CORNER CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED AND DRILLED HOLES ON NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,378 hrs · 28,035 cycles

UPPER RADIUS OF FLOORBEAM ANGLE CRACKED, RBL 9 BS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: STRUCTURE — CRACKED (BS 193) · airframe 31,384 hrs · 28,042 cycles

TRU SHELF CRACKED LT SIDE OTBD OF SERVICING GAUGE, BS 193. COMPLIED WITH REO 601R53-11-081. RECEIVED AND COMPLIED WITH REO 601R-53-2634. MAJOR REPAIR.

Part: PANEL — DAMAGED (UNKNOWN) · airframe 31,378 hrs · 28,035 cycles

PANEL 121AL HAS ERROSION DAMAGE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLETED REPAIR OF PANEL 121AL IAW SRM 51-74-02.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 31,384 hrs · 28,042 cycles

PAX DOOR SILL LOWER ATTACH ANGLE MISSING. INSTALLED SILL ANGLE IAW DWG 601R-31-527-221, 51-42-21, 51-42-13, 51-42-06, SRM 51-22-00. MAJOR REPAIR

Part: STRAP — CRACKED (RT WING) · airframe 31,384 hrs · 28,042 cycles

RT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED AND REPLACED STRAP IAW SRM 51-42-20-00 & SRM 51-42-06-00 & DWG 601R10336.

Part: FLASHLIGHT — INTERMITTENT (COCKPIT) · airframe 31,139 hrs · 27,764 cycles

CAPTAIN`S FLASHLIGHT GOES IN AND OUT. R & R FLASHLIGHT IAW AMM 25-61-02.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,329 hrs · 25,914 cycles

CABIN CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT AT 4-5CD IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: WIRE — DAMAGED (OVERHEAT DETECT) · airframe 27,157 hrs · 23,605 cycles

LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED. REPAIRED WIRE AT LT PYLON IAW ESPM 20-16-00, PERFORMED OPS TEST OF BLEED LEAK DETECTION SYS IAW AMM 36-21-00-710-801. NO FAULT AT THIS TIME.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 27,086 hrs · 23,527 cycles

AFT CORNER OF ASD ON HINGE END IS CORRODED. REMOVED AFT CORNER OF ASD AT HINGE END CORRODED. INSTALLED AFT CORNER OF ASD HINGE END IAW SRM 51-42-06, 51-42-13. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 27,086 hrs · 23,527 cycles

FWD CORNER OF ASD CORRODED ON HINGE END. R & R BOTTOM FWD CORNER OF ASD PAN. REMOVED OLD BOTTOM FWD CORNER ANGLES 2 EA DRILLED & LOCATED NEW CORNER ANGLES 2 EA IAW SRM 51-40-11. INSTALLED FWD ASD CORNER IAW SRM 51-42-06, 51-42-13. INSTALLED 3 EA FASTENER THROUGH CORNER IAW SRM 51-42-13 AND RESTORED FINISH IAW SRM 51-21-06. REPAIR CLASSIFIED AS MAJOR.

Part: UNKNOWN — CORRODED (BS 574-605) · airframe 27,086 hrs · 23,527 cycles

LBL 27 HAS CORROSION FS 605.00 TO 574.00. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS, REMOVED FLOORBEAM TEE IAW SRM 51-42-06 & 51-42-21. INSTALLED IAW REO 601R-53-61-3778, STEPS 1-4 AND STEPS 6 THRU 9.

Part: BULKHEAD — CRACKED · airframe 27,086 hrs · 23,527 cycles

REAR PRESSURE BULKHEAD CRACKED AT LBL 27.50 BETWEEN WL 121.93 & WL 137.50. REPAIRED IAW REO 601R-53-61-1541.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 27,086 hrs · 23,527 cycles

SERVICE DOOR SILL FWD ATTACH ANGLE CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE IAW SRM 51-42-21 AND DWG NR 601R38338.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,086 hrs · 23,527 cycles

CORROSION ON SERVICE DOOR SILL. REMOVED CORROSION. REMOVED .015" OF MATERIAL .048" REMAINING SILL IS OUT OF LIMITS. REPLACED SILL ANGLE. INSTALLED SILL IAW SRM 51-42-21 AND 51-42-34.

Part: SILL — CORRODED (BS 295-310) · airframe 27,086 hrs · 23,527 cycles

RT FLOOR SILL BETWEEN FS 295 AND 310 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. BLENDED AREA REQUIRES NDT THICKNESS CHECK TO DETERMINE SERVICEABILITY. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING IS .061", ORIGINAL IS .063" MATERIAL REMOVED IS .002". BLENDED AREA FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL SURFACE FINISH IAW SRM 53-00-00 AND 51-25-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,086 hrs · 23,527 cycles

ANGLE CRACKED AT RBL 9 FLOORBEAM AT FS280. REMOVED CRACKED ANGLE IAW SRM 51-42-20. LOCATED AND DRILLED NEW ANGLE. INSTALLED ANGLE IAW SRM 51-42-20.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,086 hrs · 23,527 cycles

ANGLE CRACKED AT LBL 9 FLOORBEAM AT FS 280. REMOVED CRACKED ANGLE IAW SRM 51-42-20. LOCATED AND DRILLED NEW ANGLE. INSTALLED ANGLE IAW SRM 51-42-20.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 27,086 hrs · 23,527 cycles

CARGO DOOR AFT GUIDE TRACK GOUGED JUST OTBD OF UP TURN. AREA MARKED. REMOVED AFT CARGO, AFT GUIDE TRACK IAW SRM 51-42-06 AND 51-42-21. DRILLED AND COUNTERSUNK NEW AFT GUIDE TRACK IAW SRM 51-40-11-00 AND ALODINED HOLES IAW SRM 51-21-11-00. INSTALL AFT CARGO DOOR TRACK. INSTALLED AFT CARGO DOOR AFT TRACK IAW SRM 51-42-06, 51-42-21.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 27,086 hrs · 23,527 cycles

CARGO BAY RT LOWER WALL PANEL 282ARW DAMAGED AT AFT LOWER SECTION. PICK UP FASTENER HOLES WHEN REQUESTED. DRILLED ALL REQUIRED FASTENER HOLES AS REQUIRED IAW SRM 51-40-11. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 572. THE REPAIR IS CLASSIFIIED AS A MAJOR REPAIR IAW ASA SOP 5702. REPLACE/INSTALL NEW PANEL. REPAIRED WITH SERVICABLE PANEL 282ARW REFER TO JOB 8741740, OPS 2002&7002 FOR REMOVAL AND INSTALLATION. COMPLIED WITH EO 600-25-0279. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

SEAT TRACK CORRODED AT RBL 9, FS 559+16, +48, +64. BLENDED CORROSION IAW SRM 53-51-49 & 53-21-49. FOUND TO BE IN LIMITS IAW SRM 53-21-49.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 27, FS 559 +112 CORRODED. REMOVED & REPLACED CARGO TRACK IAW SRM 53-61-49 AND 51-41-02.

Part: CARGO TRACK — CORRODED (BS 554) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 27, FS 554.00 CORRODED. R & R CARGO TRACK IAW SRM 53-61-49 & 51-41-04.

Part: CARGO TRACK — CORRODED (BS 605) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 9 FS 605.00 CORRRODED. R & R CARGO TRACK IAW SRM 53-61-49 & 51-41-04.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 27 559.+80 CORRODED. REMOVED AND INSTALLED NEW CARGO TRACK IAW AMM 20-21-00, TASK 20-21-00-910-801 AND SRM 53-61-49.

Part: SEAT TRACK — CORRODED (BS 513-529) · airframe 27,086 hrs · 23,527 cycles

SEAT TRACK CORRODED AT RBL 9, FS 529 - 513. BLENDED AREAS OF CORROSION IAW SRM 53-41-49 & SRM 53-21-49. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSP PROCEDURE UT-3, WITHIN ALLOWABLE LIMITS IAW SRM 53-21-49.

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK BETWEEN FS 605 - 621 LBL 9 IS CORRODED. R & R CARGO TRACK IAW SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT RBL 27 FS 559 +112 CORRRODED. R & R CARGO TRACK IAW AMM'S 53-01-11-000-802 & 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 589) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT FS 589 CORRRODED. R & R CARGO TRACK IAW AMM 20-21-00 TASK 20-21-00-910-801 AND SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT RBL 9 559.+80 CORRODED. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-61-49 AND AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 461) · airframe 27,086 hrs · 23,527 cycles

LEFT SEAT TRACK AT FS 461 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. PERFROMED UT THICKNESS INSP OF BLEND AREA IAW NDT INSP PROECEDURE UT-3. FOUND WITHIN LIMITS IAW SRM 53-21-49 4.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,086 hrs · 23,527 cycles

SEAT TRACK CORRODED AT RBL 9, FS 409.00+16 AND +64. BLENDED AREAS AND FOUND CORROSION DEPTH OF .025, OUT OF LIMITS IAW SRM 53-31-49 & SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-00-47.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 27 559.+80 CORRODED. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-61-41 AND AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

SEAT TRACK CORRODED AT LBL 9, FS 559+16. BLENDED CORROSION IAW SRM 53-51-49-53-21-49. FOUND TO BE IN LIMITS IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 27,086 hrs · 23,527 cycles

SEAT TRACK CORRODED AT LBL 9, FS 364.00. REMOVED CORROSION IAW SRM 51-21-06, PG1, PAR 3 & SRM 53-21-49. PERFORMED UT IAW MAC NDT INSPECTION PROCEDURES UT-3, MIN MATERIAL REMAINING FOR DIMENSION U IS .359", ORIGINAL IS 370", REMOVED IS .011. FOUND WITHIN LIMITS IAW SRM 53-21-49. PERFORMED EDDY CURRENT CHECK . NO INDICATINS NOTED.

Part: BRACKET — CRACKED (BS 484) · airframe 27,086 hrs · 23,527 cycles

CABLE SUPPORT BRACKET AT FS 484, LBL 27 CRACKED. REMOVED BRACKET, LOCATED AND DRILLED NEW BRACKET IAW SRM 51-42-21. INSTALLED NEW BRACKET IAW SRM 51-42-21 AND 51-23-00.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,086 hrs · 23,527 cycles

CARGO TRACK AT LBL 27 BS 559.+80 CORRODED. REMOVED AND REPLACED CARGO TRACK IAW AMM 20-21-00, TASK 20-21-00-910-801 AND SRM 53-61-49.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,529 hrs · 22,903 cycles

CEILING EMERGENCY LIGHT AT 14AB IS OUT. RELAMPED CEILING EMERGENCY LIGHT AT 14AB IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 559) · airframe 26,341 hrs · 22,690 cycles

FOUND FS 559 RT SIDE BULKHEAD WEB HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 24,901 hrs · 21,066 cycles

AFT EMERGENCY CEILING LIGHT IS INOP. R & R AFT EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD/ITEM: 1/ R & R AFT EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: PLACARD — MISSING (AIRSTAIR DOOR) · airframe 24,852 hrs · 21,009 cycles

EXIT PLACARD MISSING ON AIRSTAIR DOOR. REPLACED EXIT PLACARD ON ASD IAW CRJ200AMM 11-30-02.

Part: HANDLE — SEIZED (PAX DOOR) · airframe 24,579 hrs · 20,686 cycles

MAIN ASD OUTER HANDLE VERY HARD TO TURN TO UNLOCK AN OPEN DOOR. LUBED HANDLE AND DOOR SEALS INSPECTED DR OPERATION OK FOR SERVICE IAW AMM 52-11-01. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,599 hrs · 19,555 cycles

BOTH RT AND LT AFT EXTERIOR EMERGENCY LIGHTS INOP. R & R THE NR 4 BATTERY PACK (EMERGENCY LIGHT) REF: AMM TASK 33-51-04-000-801 AND TASK 33-51 04 400-801 OPS CHECKED GOOD.

Part: SILL — CORRODED (BS 347) · airframe 23,587 hrs · 19,540 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED AT AFT SECTION AT FS 347. INSTALLED FABRICATED ANGLE ALL WORK DONE IAW SRM 51-42-06. REINSTALLED PANEL 242CRF ALL WORK DONE IAW AMM 53-01-01-400-802. COMPLIED WITH EC/TC REO 601R-53-21-1105 AND REO 601R-53-21-1105 REV.

Part: BULKHEAD — CRACKED · airframe 23,582 hrs · 19,533 cycles

AFT PRESSURE BULKHEAD IS CRACKED LINTEL ATTACH BRACKET. INSTALLED LINTEL FITTING IAW STEP 5,13,14,19-24 KJ161732 INSTALLED SOLID RIVETS AROUND FILLER COMMON TO LINTEL FITTING AND SOLIDS THROUGH FUSELAGE FWD OF FS 621 IAW REO 601R-53-61-1230. INSTALLED FASTENERS AT WL 106.17 THROUGH INTERCOSTAL FROM FUSELAGE FRAME TO DOOR TRACK AND BELOW LINTEL FITTING ON AFT FRAME. IAW REO 601R-53-61-1230. COMPLIED WITH REMAINING STEPS- 5,15,13,14,19-24 IAW REO 601R-53-61-1230. COMPLIED WITH PRESSURE LEAK CHECK REF: AMM TASK 21-31-00-710-801. NO DEFECT NOTED.

Part: ATTACH BRACKET — CRACKED (BULKHEAD) · airframe 23,582 hrs · 19,533 cycles

AFT PRESSURE BULKHEAD IS CRACKED LINTEL ATTACH BRACKET AREA IS MARKED. PERFORMED CUTOUT TO AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1230, FABRICATED -3 & -4 SHIMS OUT OF 2024-T3 .020 TO A RUFF CUT, MADE CUTOUT ON INTERCOSTAL IAW REO 601R-53-61-1230. LAID-OUT PILOTED. ADDED FASTENERS ON AFT PRESSURE BULKHEAD IAW REO 601R-53-01-1230, C PG 6 FIG 3 VIEW D-D. STEP-UP ONE FASTENER HOLE ON A/C SKIN BETWEEN FS 621.00 & FS 625.00 (GROUP OF 5 HOLES) IAW SRM 51-42-21 PG 17, STEP 8. FABRICATED & INSTALLED -6 SHIM -5 FALSE FLANGE,-11 CLIP ON INTERCOSTAL IAW REO 601R-53-61-1230 REV C.

Part: ATTACH BRACKET — CRACKED (AFT PRESS BLKHD) · airframe 23,582 hrs · 19,533 cycles

AFT PRESSURE BULKHEAD IS CRACKED LINTEL BRACKET. CONTINUE FAB AND DRILLING UP REPAIR PARTS IAW REO 601R-53-61-1230 REV C. PERFORMED ET INSP OF CUT LINES ON AFT PRESSURE BULKHEAD AND INTERCOSTAL IAW REO 601R-53-61-1230 STEP 7 IAW NDTM PART 1, 51-20-06 NO INDICATIONS NOTED. COMPLIED WITH STEPS 1,2,3,4 AND 7 IAW REO 601R-53-61-1230.

Part: SILL — CORRODED (BS 349) · airframe 23,587 hrs · 19,540 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED AT AFT SECTION AT FS 349. INSTALLED TWO LOCK FASTENERS ON SERVICE DOOR ANGLE, AND RESTORE FINISH PER REO601R-53-21-1105 COMPLIED WITH STEP 5. INSTALLED 3 NUTPLATES, INSTALLED NYLON DOUBLER, INSTALLED 2 BRACKETS, AND INSTALLED LIGHTING PROTECTION PANEL PER SRM 51-41-02, 51-42-13, AND 51-42-15.

Part: ATTACH BRACKET — CRACKED (BULKHEAD) · airframe 23,582 hrs · 19,533 cycles

AFT PRESSURE BULKHEAD IS CRACKED ABOVE LINTEL ATTACH BRACKET, AREA IS MARKED. REMOVED ALL ANGLES AND BRACKETS FWD OF FS 621 BULKHEAD NESSESARY FOR LINTEL FITTING REPAIR IAW SRM 51-42-21 AND 51-42-06 FOR REO 601R-53-61-1230. PARTS ORDERED FOR FWD SIDE. REMOVED INTERCOSTAL WITH ANGLES, MADE CUTOUT ON LINTEL CHANNEL DOUBLER THEN DROPED LINTEL FITTING DOWN TO FACILITATE BULKHEAD CUTOUT IAW REO 601R-53-61-1230. CUTOUT TO LINTEL CHANNEL DOUBLER REQUIRES NDT. PERFORMED ET INSP OF CUTOUT ON LINTEL CHANNEL DOUBLER IAW EC/TC (TC REO 601R-53-61-1230 STEP 5 PER NDTM PART 1,51-20-06 NO INDICATIONS NOTED AT THIS TIME.

Part: LOCK PIN — LACK OF LUBE (ESCAPE HATCH) · airframe 23,582 hrs · 19,533 cycles

CREW ESCAPE HATCH FUNCTIONAL TEST FAILS STEPS 1B AND 1H AND STEP I OF WC ASA-2-838008. CLEANED AND LUBRICATED CREW ESCAPE HATCH LOCK PINS IAW AMM SUB TASK 12-20-52-640-003 STEP A. COMPLIED WITH FUNCTIONAL TEST OF CREW ESCAPE HATCH AND FUNCTIONAL TEST GOOD IAW AMM TASK 52-22-00-720-801.

Part: SKIN — CORRODED (BS 349) · airframe 23,582 hrs · 19,533 cycles

CORROSION ON AFT LOWER CONER OF PAX DOOR CUT OUT BELOW ANCHOR FITTING FS 349. BLENDED OUT CORROSION. ABOVE WORK PERFORMED IAW SRM 54-42-13 AND 51-21-06. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA ON BEAM AT FS 349.00 BETWEEN LBL 45.00 AND LBL 27.00 IAW MAC NDT INSP PROCEDURE UT.3. MINIMUM THICKNESS IS .057" AT LBL 45.00 AREA IS MARKED. FOUND TO BE WITHIN LIMITS REF SRM 53-21-15 FIGURE 5 PAGE 15 AND SRM 53-00-00 FIG. 102 PAGE 106. ALODINE, PRIMED & PAINTED AREA REF SRM 51-51-16 INSTALLED NYLON CAP WET & INSTALLED BRACKETS REF SRM 51-42-13.

Part: COUNTERBALANCE — OUT OF ADJUST (PAX DOOR) · airframe 23,582 hrs · 19,533 cycles

PASSENGER DOOR EXTREMELY HARD TO OPEN USING EXTERNAL HANDLE. INSPECTED AND FOUND EXTERNAL HANDLE HARD TO ROTATE NEEDS FURTHER TROUBLE SHOOTING. NEEDS MORE TROUBLE SHOOTING. UPON FURTHER TROUBLESHOOTING FOUND PAX DOOR COUNTERBALANCE OUT OF ADJUSTMENT. ADJUSTED PAX DOOR COUNTERBALANCE IAW AMM 52-11-17-820-801. OPS CK GOOD.

Part: BRACKET — DAMAGED (PROX SENSOR) · airframe 23,566 hrs · 19,515 cycles

AFTER T/O RECEIVED NOSE DOOR, GEAR DISAGREE WARNING WOW INPUT AND NOSE STEERING INOP CAUTION. RAN QKH - RETURNED TO DEPARTURE, NORMAL- LANDING HELD NOSE OFF- BELOW 80 KNOTS HAD SEVERE VIBRATION FROM NOSE. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED. FOUND NLG OLEO CENTERED/EXTENDED SENSOR BRACKET BENT. R & R BRACKET IAW CMM 32-30-04 ADJ SENSOR IAW 32-61-05 OPS CHECKED IAW 32-30-00 OPS CK NORMAL. SRM USED FOR REPAIR.

Part: STEP — CRACKED (ASD) · airframe 23,201 hrs · 19,099 cycles

ASD BOTTOM STEP CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,090 hrs · 18,977 cycles

ANGLE FOUND TO BE CRACKED UPON REMOVAL. INSTALLED NEW ANGLE AT LBL36.20 ON ENG BEAM PER SRM 51-42-06 AND 51-42-21.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,894 hrs · 18,779 cycles

FLT 5142. STRONG ODOR REPORTED BY F/O WHILE HOLDING IN ATL AIRSPACE, STRONG ENOUGH TO MAKE CREW FEEL UNCOMFORTABLE. INSPECTED CARGO COMPARTMENT AND CABIN FOUND ODOR RESEMBLING FINGERNAIL POLISH AROUND ROW 1 C/D IN CABIN, ODOR DISAPEARED SHORTLY AFTER GROUND AIR WAS CONNECTED TO ACFT, REMOVED CABIN EMERGENCY EXITS, VENTALATED ACFT FOR 30 MIN. REPLACED EMERGENCY EXITS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,539 hrs · 18,411 cycles

CAPT`S FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,518 hrs · 17,469 cycles

EMERGENCY LIGHTS DON’T COME ON.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,928 hrs · 16,024 cycles

FWD EMERGENCY LIGHTS INOP.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 19,639 hrs · 15,789 cycles

PAX DOOR FWD STAIR ANGLE CRACKED IN RADIUS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

FUSELAGE FRAME AT FS 349.0 HAS CORROSION AT BL 0. REMOVED CORROSION, DAMAGE FOUND WITHIN LIMITS IAW SRM 51-21-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - BATH TUB FITTING AT FS 461, RBL 9, CRACKED. REMOVED UNSERVICEABLE BATH TUB FITTING . LOCATED HOLES IN NEW FITTING, IAW SRM 51-42-11. OK TO INSTALL INSTALLED NEW SERVICEABLE FITTING PER SRM 51-42-21. OK TO FILLET SEAL AND TOUCH-UP FINISH. APPLIED FILLET SEAL PER SRM 51-23-00 AND TOUCHED-UP FINISH A023 PER SRM 51-21-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - FUSELAGE FRAME AT FS 333.0 HAS CORROSION BL 0 TO LBL 9.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - FS 484 CLIP CRACKED I/B LBL 27.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - FS 484 CLIP CRACKED I/B RBL 27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

FS 280 AFT ANGLE CRACKED O/B OF LBL 9. PERFORMED REPAIR TO FS 280.0 AFT ANGLE IAW REO 601R-53-11-136. REV A. COMPLIED WITH EO 600-53-0091.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - FS 280 FWD FLOOR ANGLE BETWEEN LBL 9.0 & RBL 9.0 HAS MINOR SURFACE CORROSION. REMOVED FWD FLOOR ANGLE TO FACILITATE CORROSION REMOVAL. REMOVED MINOR CORROSION TO 0.003" ON FWD FLOOR ANGLE AT F.S. 280.0 LBL9 TO RBL9. RETURNED TO FINISH CODE A023. WORK ACCOMPLISHED IAW SRM 51-21-06, 51-21-11, 51-25-06, AND 51-25-16. OK TO REINSTALL FWD FLOOR ANGLE. REINSTALLED FWD FLOOR ANGLE IAW SRM 51-42-06.

Part: WEB — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

AAR - FS 280 LOWER WEB CRACKED O/B OF RBL 9 (MARKED).

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 19,639 hrs · 15,789 cycles

FS 280 ATTACH FITTING O/B RBL 9 CRACKED. REMOVED CRACKED FS 280 ATTACH FITTING. FABRICATED AND INSTALLED SERVICEABLE ATTACH FITTING IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 19,639 hrs · 15,789 cycles

RT WHEEL WELL I/B BATT RIB ATTACH ANGLE CRACKED

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 19,639 hrs · 15,789 cycles

FS 280 ATTACH FITTING O/B LBL 9 CRACKED. REMOVED CRACKED F/S 280 ATTACH FITTING. FABRICATED AND INSTALLED SERVICEABLE ATTACH FITTING IAW SRM 51-42-21.

Part: SIGN — MISSING (CABIN) · airframe 19,639 hrs · 15,789 cycles

SIGN MISSING ON LEFT OF PAX DOOR.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,268 hrs · 14,718 cycles

CAPT'S, F/O'S, AND F/A'S FLASHLIGHT INOP AND DIM.

Part: DOOR — OBSTRUCTED (MAIN PAX) · airframe 18,165 hrs · 14,643 cycles

PAX DOOR WILL NOT CLOSE, IT GETS 18 INCHES FROM AIRFRAME AND STOPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,782 hrs · 14,348 cycles

FLOOR PROXIMITY LIGHTING INOP ROW 10-14. FLT 4129 DEL 40 MINS. ELECTROLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,697 hrs · 14,270 cycles

FLOOR EMERGENCY LIGHTS AFT OF OVERWING EXIT ARE INOP. FLT 4722 DEL 165 MINS.

Part: DOOR — UNKNOWN (PAX DOOR) · airframe 17,253 hrs · 13,947 cycles

PAX DOOR HARD TO OPEN.

Part: WARNING MESSAGE — ACTIVATED (HYDRAULIC SYS) · airframe 17,219 hrs · 13,915 cycles

HYD SYS 2 LO PRESS MSG, HYD SYS 2 QTY INDS ZERO. EN ROUTE TO HSV, A/C DIVERTED TO GSO DUE TO MTC. EMERGENCY DECLARED. FLTS 4539, 4586 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,069 hrs · 13,797 cycles

FOUND FWD EMERGENCY EXTERIOR OVERWING EXITING LIGHTS INOP. BOTH SIDES.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 16,582 hrs · 13,425 cycles

ASD FWD ANCHOR FITTING APPEARS TO BE CRACKED.

Part: YOKE — VIBRATION (COCKPIT) · airframe 15,950 hrs · 12,923 cycles

AT AN ALTITUDE OF 10000 FT, FELT A VIBRATION ON THE LEFT YOKE. WITH A AIRSPEED OF 290 KIAS. RECEIVED A TURN TO CAE AND ON THE APPROACH WITH THE AUTOPILOT OFF IT HAPPENED AGAIN. A/C RETURNED TO CAE AFTER T/O, EMERGENCY WAS DECLARED, FLTS 4321, 4586 CX.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 15,753 hrs · 12,764 cycles

NWS INOP MSG AFTER TAKEOFF COMPLIED WITH QRH, LANDED WITH NWS OFF, FLT 4613 DEL 63 MINS (AN EMERGENCY WAS DECLARED).

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,652 hrs · 12,679 cycles

DURING FRAME 640 INSP, FOUND RIGHT RE-ENFORCEMENT BRACKET CRACKED AT 640 FRAME.

Part: SMOKE WARNING — ILLUMINATED · airframe 15,181 hrs · 12,312 cycles

SMOKE CARGO MESSAGE IN FLIGHT... A/C RETURNED TO ATL AFTER T/O... A/C SWAP TO 699, FLT 4552 DEL 114 MINS (AN EMERGENCY WAS DECLARED)

Part: FITTING — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 484, LBL 27 AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 21 IN THE CARGO COMPARTMENT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M0

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 TO FS 605 IAW ASA EO 600-53-0117. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4887 - DUIRNG A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY LIGHTS AT ROWS FIVE AND FOURTEEN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT LAMPS AT ROWS FIVE AND FOURTEEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

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

Part: STEP — CRACKED (FUSELAGE)

DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR)

FLT 4236 - DURING A GROUND INSPECTION IN ATL, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM OUTSIDE WITH THE HANDLE. MAINTENANCE LUBRICATED THE MAIN PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FIRE LOOP — INOPERATIVE (LT ENGINE)

FLT 4766 - DURING CLIMB-OUT DFW-AUS, THE CREW RECEIVED A LEFT ENGINE 14TH STAGE DUCT MESSAGE AT APPROXIMATELY 14,000 FEET. QRH AND EMERGENCY PROCEDURES WERE COMPLIED WITH. THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE 14TH STAGE PYLON FIRE LOOP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4042 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 2 THROUGH 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLEXIBLE LAMP STRIP BETWEEN ROWS 2 THROUGH 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — CRACKED (RT WING)

DURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL REPLACE THE RIGHT WING TRAILING EDGE RIB. (M)

Part: FITTING — CRACKED (RT WING)

DURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AILERON INBOARD CLOSURE RIB IAW SRM 51-00. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4423 - DURNG DESCENT INTO OMA, THE FIRST OFFICERS WINDSHIELD CRACKED. NO EICAS MESSAGE WAS RECEIVED, BUT THE WINDSHIELD FELT COLD. THE CAPTAIN REPORTED ALL HEAT SWITCHES WERE IN THE CORRECT POSITIONS. AIRCRAFT LANDED SAFELY IN OMA. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (CABIN)

FLT 4496 - CAPTAINS FRONT WINDSHIELD CRACKED WHILE ON THE GROUND AFTER FLIGHT FROM DFW TO CHS. MAINTENANCE REMOVED AND REPLACED CAPTAINS FRONT WINDSHIELD. HEATING AND PRESSURIZATION TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)