N652BR

Part: A/C PACK — FAILED (RIGHT) · airframe 41,481 hrs · 35,612 cycles

WHILE CLIMBING THROUGH 23000 FT RIGHT PACK TURNED OFF. RAN CHECKLISTS AND DESCENDED TO 15000. DO TO THE TERRAIN AND NOT BEING ABLE TO GET LOWER THE PASSENGER MASKS DEPLOYED AND CABIN HIGH ALT OCCURRED. (FLIGHT 5488 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23485999 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE THE FOLLOWING CAMP ITEMS FOR MX PERFORMED. CP23485989, CP 23485991, CP 23485992, CP 23485993, CP 23485994, CP 23485995, CP 23486581, CP 23486142, CP 23487746. CP 23503785. OPERATIONAL CHECK OF RT PACK GOOD WITH NO FAULTS NOTED. REPLACED PAX O2 MASKS AND O2 GENERATORS AS NEEDED. OPERATIONAL CHECK OF O2 MASK DEPLOY SYSTEM GOOD.

Part: SKIN — DAMAGED (BS 265-280) · airframe 41,217 hrs · 35,390 cycles

AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 265.00 - FS 280.00 BETWEEN STR 25L AND STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS265.00 - FS280.00 AND STR24L - STR25R IN REF TO REO 601R-53-11-3715, REV--, DATED 2021-07-21. COPLIED WITH TASK CARD 51-900-1003-SKY AND M-337

Part: SKIN — DAMAGED (BS 235 S25-26L) · airframe 41,217 hrs · 35,390 cycles

AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN AND REPAIR DOUBLER AT FS 235.00, BETWEEN STR 25L - STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS227.74 - FS250.00 AND STR24R - STR24L IN REF TO REO 601R-53-11-3714, REV--, DATED 2021-07-21. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337.

Part: APU — SHUTDOWN

APU INFLIGHT SHUTDOWN WHILE ENROUTE. SINGLE GENERATOR. VERIFIED APU INTAKE DOOR CLOSED AND ALL MX ACTION HAS BEEN COMPLIED WITH. REACTIVATED APU PER MEL 49-10-1A TROUBLESHOT APU INFLIGHT SHUTDOWN IAW FIM 49-10-00. REMOVED AND REPLACED APU ECU IAW AMM 49-61-01. OPS CHECK GOOD AT THIS TIME. PLACARDS REMOVED DMI CLEARED.

Part: BRACKET — BENT (WOW SENSOR) · airframe 41,063 hrs · 35,241 cycles

GEAR DISAGREE EMERGENCY MESSAGE. NOSE GEAR REMAINED DOWN. RAN QRH AND EXTENDED ALL GEAR SUCCESSFULLY AND COMPLETED RTF. (FLIGHT 5289 - FILED CLOSED) FOUND NOSE LANDING GEAR WOW SENSOR BRACKET BENT, REPLACED BRACKET AND ADJUSTED WOW SENSOR IN REFERENCE TO CRJ 200 MM 32-61-04, NOSE GEAR STILL NOT RETRACTING, PER FIM REPLACED NOSE LANDING GEAR SELECTOR VALVE IN REFERENCE TO CRJ 200 MM 32-33-10, GEAR CYCLES NORMALLY.

Part: HEAT SHIELD — CRACKED (APU EXHAUST) · airframe 40,156 hrs · 34,419 cycles

APU HEAT EXHAUST SHIELD HAS A CRACK BETWEEN THE 7 O`CLOCK AND 8 O`CLOCK POSITION. FILED CLOSED RO 10/5/2020. REMOVED AND REPLACED APU HEAT EXHAUST SHIELD, IN REF TO CRJ200 AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 & FS672.20 AND STR 1R - STR 2R REQUIRES REPAIR. (C-CHECK) RO 4/27/2020 REPAIRED FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 - FS672.20 AND STR 1R - STRG 2R REF REO.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

WHILE PERFORMING REPLACEMENT OF RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128, FOUND 4 EACH HOLES ELONGATED ON BULKHEAD WEB AND 1 EACH DENT. (C-CHECK) RO 4/27/2020 REPAIR DAMGED AT RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128 REF REO. COMPLIED WIT STEPS OF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

DENTS FOUND IN MULTIPLE LOCATIONS ON TOP SIDE OF FUSELAGE BETWEEN FS 621.00 AND FS 755.00 PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 REWORKED AND REPAIRED ALL TOP SIDE FUSELAGE SKIN DENTS. REF REO, AND REO. REFERENCE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD. WEIGHT REMOVED/INSTALLED NEGLIGABLE.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FLOORBEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3) REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 REMOVED THE DAMAGED BEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3), REF SRM. INSTALLED NEW BEAM CAP P/N 601R35031-3 FROM FS569 TO FS621 LBL27 REF SRM 51-42-21, REO AND DWG. REFERENCE THE CONTINUE CARD FOR DETAILS. OPERATIONAL CHECKS GOOD.

Part: STRAP — WORN (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT STRAP FS559.0 RBL 40 AND 27 APPROX REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 ORDERED AND RECEIVED, DRILLED AND LOCATED NEW PART, INSTALLED NEW STRAP ON THE RT SIDE AT FS559.00 RBL 27 - 40. REF SRM, DRAWING. COMPLIED WITH TASK CARD.

Part: POST — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS 409+128 LBL 18.0 OUTBD VERTICAL POST AFT RADIUS IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED 2 EA PLATES ATTACHED TO VERTICAL STIFFENER FS 409+128 LBL18 AT WL 65.90 & WL 53.42 FOM. REF SRM. REMOVED I/B STIFFENER AND O/B CRACKED STIFFENER OF OUTBOARD VERTICAL POST AT FS 409.00+128, LBL 18.0 FOR THE FOM. REF SRM. INSTALLED I/B STIFFENER AND NEW O/B STIFFENER OF OUTBOARD VERTICAL POST AT FS 409.00+128, LBL 18.0, REF REO AND DWG. INSTALLED 2 EA. PLATES TO VERTICAL STIFFENER FS 409+128 LBL18 AT WL 65.90 & WL 53.42. REF SRM DWG. RESTORED FINISH AND CIC.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS 409+128 BL 0.0 RT VERTICAL POST UPPER STIFFENER IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT VERTICAL POST AT BL 0.0 FS 409.00+128 INSTALLED REF SRM AND DRAWING.

Part: POST — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST HAVE CRACKS IN AFT RADIUS. (C-CHECK) RO 4/27/2020 REMOVED AND INSTALLED NEW FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST. REF DWG, REO AND SRM. ALL CHECKS GOOD AT THIS TIME.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE AVIONICS BAY DOOR SURROUND AFT LT GUIDE FITTING IS BROKEN/CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED WITH NEW1 EACH AFT LT GUIDE FITTING ON AVIONICS BAY DOOR REF SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE FRAME AT FS349.00 HAS CORROSION FROM STRINGER 26R TO 26L. (C-CHECK) RO 4/27/2020 BLENDED OUT CORROSION ON LOWER FRAME SECTION AT FS349 FROM STR 26R TO 26L. REF SRM. ORIGINAL MATERIAL THICKNESS IS .063" PER SRM. MATERIAL LOSS IS .005 WITH .058" REMAINING. DAMAGE IS OUT OF LIMITS PER SRM FOR DAMAGE EXTENDING MORE THAN 30 PERCENT OF PART AND DAMAGE COVERS MORE THAN ONE ELEMENT AT A CROSS SECTION. INSTALLED NEW LOWER FRAME SECTION P/N 601R32005-69 AT FS349 FROM STR 23L - STR 23R. REF SRM, DWG. PRESSURE CHECKS GOOD AT THIS TIME. REFERENCE THE CONTINUE CARD FOR WORK PERFORMED.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE AVIONICS BAY DOOR CUTOUT SURROUND FWD LT STOP FITTING IS CHAFFED. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT LIMITS REF SRM. REMOVED AND REPLACED NEW AVIONICS BAY DOOR CUTOUT SORROUND FWD LT STOP FITTING. REF SRM.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING IS CHAFED. (C-CHECK) RO 4/27/2020 REPLACED AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING REF SRM TUC4200 DUE:30-SEP-20 SEE CONTINUE CARD FOR WORK PERFORMED.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE PRESSURE FLOOR SKIN BETWEEN LBL 9.00 AND BL 0 AT APPROX FS 461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.06LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.36LB. PRESSURE CHECKS GOOD AT THIS TIME.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS559.00+112 - 621.00 SEAT RAIL BEAM CAP AT LBL27 CORRODED IN NUMEROUS AREAS. (C-CHECK) RO 4/27/2020 REMOVED CORROSION FROM SEAT RAIL BEAM CAP AT LBL27 FS559.00+112 - 621.00. BLEND OUT AT FLOORBEAM FS559+112 - FS569.00, INBD LBL27 WAS FOUND TO BE WITHIN LIMITS, REF REO. BLEND OUT ON FLOORBEAM CAP AT FS569.00 - FS621 LBL27 WAS FOUND TO BE OUT OF LIMITS. REF REO AND DWG. FLOORBEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3) REPLACED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE CROSSBEAM CAP AT FS559.00+48 BETWEEN RBL27.00 AND RBL9.00 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE FLOOR SUPPORT PLATE. REF SRM, DRAWING.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED RT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD AT THIS TIME.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT GALLEY OUTBRD DOUBLER PLATE APPROX FS 319 RBL 35 HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED O/B DOUBLER PLATE AT FS319 AND RBL 35 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

LT FS 484 INBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 INBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 INBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-2 REF PREVIOUSLY INCORPERATED RE. INSTALLED LT FS484 OUTBOARD PULLEY ANGLE BRACKET. PRESSURE CHECKS GOOD AT THIS TIME.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

SERVICE DOOR SILL HAS CORROSION RT FS 319- 349. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW MID SUPPORT ANGLE P/N 601R38303-253 AT RT FS319.00 TO FS 349.00 REF SRM AND DRAWING.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE PRESSURE FLOOR SKIN BETWEEN RBL 9.00 AND BL 0 AT APPROX FS461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.05LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.37LB. PRESSURE CHECKS GOOD AT THIS TIME.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS559.00+112 - 574.00 (APPROXIMATE) AT LBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED SEAT TRACK FROM FS559+112 -FS574 LBL9 REF SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FS559.00+112 - 574.00 (APPROXIMATE) AT RBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM 53-61-49. REMOVED AND INSTALLED NEW CARGO SEAT TRACK INSTALLED ATFS 559.00+112 TO FS 574.00 AT RBL 9.0 REF AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 RBL 9. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE RT FLOORBEAM AT RBL 9 BETWEEN FS409.00+05 TO 409.00+121. REF REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE SEAT TRACK SECTION FROM APPROX FS559.00 TO FS559.00+80 AT RBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW PASSENGER FLOOR SEAT RAIL AY FS 559.00 TO 559.00+80 RBL 9.0 REF AMM AND REO. COMPLIED WITH ALL STEPS OF REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT STRAP FS559.0 LBL 40 AND 27 APPROX HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION AND RT STRAP FS559.0 WAS FOUND TO BE OUT OF LIMITS REF SRM. REPLACED ON MX#20971547, JOB 2742971. SEE CONTINUTION CARD FOR DETAILS.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

LT STRAP FS559.0 LBL 35 AND 27 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION ON LT STRAP AT FS559 BETWEEN LBL27 - LBL35 REF SRM. LT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 35 HAS AN ORIGINAL THICKNESS OF 0.050? REF SRM 53-41-43 FIG 1. MIN REMAINING THICKNESS MEASURED IS 0.026?. MATERIAL LOSS IS 0.024?. MAXIMUM MAT LOSS ALLOWABLE IS .005? REF SRM. CORROSION REMOVAL IS OUT OF LIMITS. REPLACED STRAP P/N 601R31025-29 FS 559.00 LBL 35 AND 27 REF SRM. PRESSURE CHECKS GOOD AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT FLOORBEAM FS 409.00+128 TO 599.0 RBL 9 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED THE CORROSION, ENSURED REMAINING MATERIAL THICKNESS (NDT) - FOUND OUT OF LIMITS. RECEIVED ENGINEERING SUPPORT, COMPLIED WITH REO - PART IN LIMITS. REF REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

THE LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED LT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, AND REO. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD AT THIS TIME.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

LT FS 484 OUTBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 OUTBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 OUTBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-1 REF: PREVIOUSLY INCORPERATED REO. INSTALLED LT FS484 OUTBOARD PULLEY ANGLE BRACKET REF REO. PRESSURE LEAK CHECKS GOOD AT THIS TIME.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT GALLEY INBRD FWD DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED FWD DOUBLER PLATE AT FS295 AND RBL 4.25 REF SRM AND DWG. SEE CONTINUATIO CARD FOR DETAILS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT GALLEY INBRD AFT DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED AFT DOUBLER PLATE AT FS324 AND RBL 4.25 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

LT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 LBL 9. (C-CHECK) RO 4/27/2020 BLENDED CORROSION ON LT FLOOR BEAM AT FS409.00+05 TO FS409.00+121 REF. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH TASK CARD.

Part: CONNECTING ROD — CHAFED (RT MLG) · airframe 39,794 hrs · 34,058 cycles

RT MLG LWR/OTBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF INBD END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REMOVED RT MLG DOOR STRUT. REF AMM - INSTALLED NEW RT MLG DOOR STRUT (WITH ONE EACH NEW BOLT, ONE NEW WASHER AND ONE NEW NUT AT THE DOOR SIDE). REF AMM. ADJUSTMENT CHECKS GOOD. OPS TEST GOOD.

Part: CONNECTING ROD — CHAFED (RT MLG) · airframe 39,794 hrs · 34,058 cycles

RT MLG UPPER/INBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF LWR END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REPLACED RT MLG DOOR PUSH/PULL ROD REF AMM. OPS TEST GOOD.

Part: SUPPORT — CHAFED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKHEAD FS 621.00, BL 0.00, IS CHAFED FROM MECHANICAL CONTACT WITH 10TH STAGE BLEED AIR SOV APROX 10' FROM TOP OF POST. (C-CHECK) RO 4/27/2020 REPAIRED CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKHEAD FS 621.00, BL 0.00, ALL STEPS COMPLIED WITH REO.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FOUND CRACKED ATTACHING (CLIP) AFT LT SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14L LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACHING (CLIP) AFT LT SIDE OF REAR PRESSURE BULKHEAD FS621.00 THAT ATTACHES TO FS625.00 BY COMMON INTERCOSTAL AT APPROX STR 14L LEVEL REF SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

FOUND CRACKED ATTACHING (CLIP) AFT R/H SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14R LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACHING (CLIP) AFT RT SIDE OF REAR PRESSURE BULKHEAD FS621.00 THAT ATTACHES TO FS625.00 BY COMMON INTERCOSTAL AT APPROX STR 14R LEVEL REF SRM.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

SMALL SECTION OF STRINGER ATTACHED TO AFT PRESSURE BULKHEAD FS 621.00 THAT SPANS FROM THE AFT CARGO DOOR AFT TRACK OTBD TO FS 621.00, FOUND GOUGED/BENT FROM PROBABLE PREVIOUS MECHANICAL CONTACT WITH AFT CARGO DOOR AFT LOCK BOLT. (C-CHECK) RO 4/27/2020 REMOVED GOUGE/BENT DAMAGE TO ANGLE ATTACHED TO AFT PRESSURE BULKHEAD AT FS621.00 WL 120.43, LBL39 REF SRM. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUE CARD FOR DETAILS.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

(AFT) ATTACHING ANGLE (BOTTOM SIDE) AT FS 621.00 AND COMMON TO THE PRESSURE BULKHEAD, FOR ATTACHMENT OF THE CARGO DOOR CAM TRACK SUPPORT ASSY FOUND CRACKED. (C-CHECK) RO 4/27/2020 REPLACED CRACKED AFT ATTACHING ANGLE WITH NEW ONE P/N 601R35050-109 AT FS 621.00 AT BOTTOM SIDE COMMON TO PRESSURE BULKHEAD AND CARGO CAM TRACK SUPPORT REF SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RT FUSELAGE SKIN HAS DENT OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT APPROX FS 232 / BL 8 RT. (C-CHECK) RO 4/27/2020 REPAIRED THE DENT AT THE RT FUSELAGE SKIN, OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT. REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,794 hrs · 34,058 cycles

LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584FT. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E OUTBOARD SECTION WITH NEW PN 601R14303-43 PO# T-54677 REF DWG AND SRM. COMPLIED WITH CARD.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,794 hrs · 34,058 cycles

RT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684FT. (C-CHECK) RO 4/27/2020 REPLACED RT INBOARD FLAP VANE SKIN OUTBOARD OF PANEL 684FT PN 601R14303-44S REF DWG SRM, SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,794 hrs · 34,058 cycles

RT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684ET. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT I/B FLAP VANE SKIN (CAP) OUTBOARD OF PANEL 684ET REF SRM AND DWG.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,794 hrs · 34,058 cycles

RT INBOARD FLAP VANE SKIN IS CHAFED INBOARD OF PANEL 684DT. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT I/B FLAP SKIN (CAP) INBOARD PANEL 684DT REF SRM AND DWG.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,794 hrs · 34,058 cycles

LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584ET. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E CENTER SECTION WITH NEW PN 601R14303-51 PO# 7426-00010 REF DWG AND SRM. COMPLIED WITH CARD.

Part: SKIN — DENTED (TE FLAP) · airframe 39,794 hrs · 34,058 cycles

LEFT OUTBD FLAP. DENT MEASURING L=0.8" W=0.69" D=-.035". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 REPAIRED THE LEFT OUTBOARD FLAP REF SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

RIGHT SIDE FUSELAGE APPROXIMATELY AT 7 O'CLOCK POSITION. BETWEEN FS364.00 & FS379.00. DENT LOCATED BELOW AND SLIGHTLY AFT OF FWD POTABLE WATER SERVICE PANEL. DENT MEASURES 2.5" W X 2.5" L WITH A MAXIMUM DEPTH OF 0.078" AT THE DEEPEST POINT. W/D = 32.05. REQUIRED TO BE GREATER THAN 25. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 PERFORMED HAND DRESS BACK OF SKIN DENT LOCATED BETWEEN FS 364.00 AND FS 379.00, AFTER REFORMED TO ORIGINAL CONTOUR NOTICED TO HAVE OIL CANNING EFECT, THEREFORE FOUND TO BE OUT OF LIMITS. REF; RE0. PERFORMED SKIN AND PLATING. PRESSURE CHECKS GOOD AT THIS TIME.

Part: SKIN — CRACKED (TRU DOOR) · airframe 39,794 hrs · 34,058 cycles

LT SIDE TRU SKIN CRACKED BY AFT LATCH CUTOUT. PERFORMED TEMPORARY GENERIC DISPOSITION FOR CRACK ON ELECTRONICS BAY ACCESS DOOR AFT LATCH CUT-OUT REF REO. ALL STEPS COMPLETED AT THIS TIME. PERM REPAIR DUE IN 6000 FH DUE BY 40282.4 TAT.C: MCI. NOTE: BUILT MX CODE FOR REINSP EVERY 600 HR. DO NOT CLOSE UNTIL PERMANENT REPAIR, (C-CHECK) RO 4/27/2020 REPLACED WITH NEW LT SIDE TRU SKIN REF SRM, DWG, AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 39,743 hrs · 34,020 cycles

FLAPS FAIL CAUTION MSG AFTER TAKE OFF WITH FLAPS AT ZERO FLIGHT 5227 - FILED CLOSED RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP RESET PROCEDURES AND AD MCI CREATED FOR FULL AD COMPLIANCE BY MCC.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,794 hrs · 34,058 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL, TO APPENDIX AIRWORTHINESS LIMITATIONS. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER, SERIAL NUMBER: 7429, POSITION (C-CHECK) RO 4/27/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 39,252 hrs · 33,583 cycles

PAX DOOR WARNING MSG BETWEEN 31000 AND 33000 FT. FOLLOWED QRH PROCEDURE. LANDED AT CLOSEST SUITABLE AIRPORT. MSG CLEARED ON DESCENT. PAX DOOR LATCH CAUTION MSG AT 12-8000 FT. FLIGHT 5292 CLOSED REMOVED AND REPLACED PAX DOOR PRESSURE SEAL IAW AMM OPS CHECK GOOD AT THIS TIME. NO DOOR WARNING INDICATIONS DISPLAYED AT THIS TIME. COMPLETED PRESSURE TEST AND WAS ABLE TO PREFORM TEST WITH NO FAULT INDICATION AND NO AIR LEAKS NOTED BY MX AT THIS TIME. FOUND THAT MICRO SWITCH IN PAX DOOR WAS FOUND TO BE WITHIN SERVICEABLE CONDITION. NO FARTHER DISCREPANCIES NOTED BY MX AT THIS TIME.

Part: UPLOCK — FAILED (NLG) · airframe 38,714 hrs · 33,101 cycles

ON APPROACH INTO SPI GEAR DISAGREE WARNING. A GO AROUND WAS INITIATED AND THE WARNING WENT AWAY AND NOSE GEAR INDICATED DOWN AND LOCKED. QRH PROCEDURE ACCOMPLISHED. A NORMAL LANDING WAS ACCOMPLISHED. TROUBLESHOT GEAR DISAGREE WARNING MESSAGE IAW FIM. REMOVED AND REPLACED NLG UP-LOCK ASSY IAW AMM. OPS CHECK GOOD.

Part: LANDING GEAR — SLOW · airframe 38,670 hrs · 33,060 cycles

ON APPROACH, PUT THE GEAR DOWN BEFORE THE FLAP TO LOSE SPEED. PUT THE GEAR DOWN AT APPROXIMATELY 200KIAS. GOT A HYD 3 LOW PRESS MSG FOLLOWED BY A GEAR DISAGREE MSG FOLLOWED BY A NOSE GEAR MSG. THE GEAR DID EVENTUALLY COME DOWN. WENT AROUND AND DID PUT THE GEAR UP. THE GEAR DID COME DOWN THE NEXT TIME WITH NO ISSUES. THIS TIME DID HAVE THE FLAPS DOWN FIRST. FLT 5936. INTERROGATED PSEU AND FOUND NOTHING LOGGED. PERFORMED OPS CHECK OF NOSE GEAR BY PERFORMING MULTIPLE NOSE GEAR RETRACTIONS AND EXTENSIONS IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,317 hrs · 31,841 cycles

SMALL, SHALLOW INDENTATION BELOW AFT CARGO DOOR. (SVC CHECK) RO: 11/03/2018 REPAIRED DENT IN THE FUSELAGE SKIN LOCATED BETWEEN FS559.00 + 112 - FS574.00 AND BETWEEN STR 21L - STR 22L IAW REO.

Part: NOT REPORTED — MALFUNCTIONED (LANDING GEAR) · airframe 36,784 hrs · 31,366 cycles

GEAR DISAGREE WARNING MESSAGE WHEN GEAR WAS EXTENDED. THE MESSAGE WENT AWAY ON ITS OWN. FLIGHT 3248. 3A ACMP REPLACEMENT. PERFORMED SEVERAL GEAR EXTENSION AND RETRACTION CHECK IN REFERENCE TO AMM 32-30-00. OPS CHECK GOOD AT THIS TIME.

Part: WIRE HARNESS — FAILED (ANTI-SKID) · airframe 36,536 hrs · 31,128 cycles

ANTI-SKID INBD CAUTION WHEN LANDING GEAR WAS LOWERED ON FINAL. REMOVED AND REPLACED THE RT MLG INBOARD ANTI-SKID MIDDLE ELECTRICAL HARNESS IAW AMM. OPS CHECKED GOOD.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 34,284 hrs · 28,681 cycles

REAR PRESSURE BULKHEAD FORWARD FACE ABOVE FLOOR DENT ON SKIN AT RBL18.00 42.5 INCHES ABOVE FLOOR OUT OF LIMITS. COMPLIED WITH REPAIR OF DENT ON REAR PRESSURE BULKHEAD FORWARD FACE ABOVE FLOOR ON SKIN AT RBL18.00 42.5 INCHES ABOVE FLOOR IAW REO. NO LEAKS NOTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,284 hrs · 28,681 cycles

RT PRESSURE FLOOR SILL FLOOR ANGLE AT FS 449.85 FOUND TO BE OUT OF LIMITS DUE TO CORROSION. REPAIRED RT PRESSURE FLOOR SILL FLOOR ANGLE AT FS 449.85 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,284 hrs · 28,681 cycles

LEFT CARGO FLOOR SILL HAS CORROSION AT FS589.00. REMOVED AFT CARGO DOOR FLOOR SILL AND INSTALLED NEW FROM FS580 TO FS621 IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,284 hrs · 28,681 cycles

RIGHT AILERON UPPER SURFACE LEADING EDGE IS CHAFED IN MULTIPLE AREAS. REMOVED AND REPLACED DAMAGED RT UPPER AILERON SKIN WITH NEW SKIN P/N: 601R13031-166 IAW SRM.

Part: SKIN — CHAFED (LTAILERON) · airframe 34,284 hrs · 28,681 cycles

LEFT AILERON UPPER SURFACE LEADING EDGE IS CHAFED IN MULTIPLE AREAS. REMOVED AND REPLACE LT AILERON UPPER SURFACE LEADING EDGE IAW SRM.

Part: FAIRING — CHAFED (TE FLAP) · airframe 34,284 hrs · 28,681 cycles

LT FLAP STUB FAIRING HAS CHAFING. REMOVED AND REPLACED OUT OF LIMITS LT FLAP STUB FAIRING WITH NEW LT FLAP STUB FAIRING P/N: 601R31199-91 IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,284 hrs · 28,681 cycles

PAX DOOR SURROUND STRUCTURE - KICK ANGLE, UNDER THE MID CAP ANGLE, HAS CORROSION. REMOVED AND REPLACED PAX DOOR SURROUND STRUCTURE CORRODED KICK ANGLE WITH NEW KICK ANGLE P/N: 601R31527-221 IAW SRM.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 33,910 hrs · 28,279 cycles

NOSE GEAR DISAGREE AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD. MX ADJUSTED NOSE GEAR OLEO STRUT PROX SENSOR IAW AMM. SWUNG THE GEAR SEVERAL TIMES. OPS CHECKS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 32,852 hrs · 27,226 cycles

GEAR DISAGREE NLG WITH NOSE GEAR DOOR CAUTION. ADJUSTED NOSE GEAR PROXIMITY SENSOR IAW AMM. PERFORMED GEAR SWINGS, OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-589) · airframe 29,300 hrs · 24,128 cycles

RBL 36 AT FLOOR SUPPORT FROM BS 559+96 TO 589 HAS CORROSION. BLENDED OUT CORROSION IAW REO AND SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,300 hrs · 24,128 cycles

BS 280 FLOORBEAM LOWER ANGLE CRACKED AT TWO LOCATIONS LBL 9.0 AND RBL 9.0 COMMON TO VERTICAL POST. C-CHECK, REPAIRED FLOORBEAM ANGLE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,300 hrs · 24,128 cycles

FS 280 FLOORBEAM ANGLE CRACKED AT RBL 9 OTBD. R & R THE FLOORBEAM ANGLE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,300 hrs · 24,128 cycles

BS 280 FLOORBEAM ANGLE CRACKED AT LBL 9 INBD. R & R FLOORBEAM ANGLE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,300 hrs · 24,128 cycles

FS 280 FLOORBEAM UPPER ANGLE CRACKED OTBD OF LBL 9. REPAIRED THE FLOORBEAM UPPER ANGLE IAW REO.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 29,300 hrs · 24,128 cycles

SERVICE DOOR OUTER SKIN AT HANDLE CUTOUT HAS TWO GOUGES. BLENDED SERVICE DOOR OUTER HANDLE CUTOUT IAW EA.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,300 hrs · 24,128 cycles

FS 280 FLOORBEAM ANGLE CRACKED RBL 9 INBD. R & R THE FLOORBEAM ANGLE IAW REO.

Part: HINGE — GOUGED (SERVICE DOOR) · airframe 29,300 hrs · 24,128 cycles

SERVICE DOOR HINGE HAS THREE GOUGES ON LOWER OTBD. BLENDED DOOR HINGE IAW EA.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,300 hrs · 24,128 cycles

PAX DOOR HINGE LUGS, DOOR SIDE, GOUGED ON LUG NR 22, NR 24 AND NR 26. C-CHECK, RO: 08/19/2014, BLENDED GOUGES ON PAX DOOR HINGE LUGS, DOOR SIDE, NR 22, NR 24, AND NR 26, IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,300 hrs · 24,128 cycles

PAX DOOR HINGE LUGS, FUSELAGE SIDE, GOUGED ON LUG NR 2, NR 11, NR 14 AND NR 18. BLENDED GOUGES ON PAX DOOR HINGE LUGS, FUSELAGE SIDE, NR 2, NR 11, NR 14, AND NR 18, IAW REO.

Part: SKIN — CHAFED (PAX DOOR) · airframe 29,300 hrs · 24,128 cycles

PAX DOOR EXTERIOR SKIN AROUND DOOR HANDLE CHAFED. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 461-559) · airframe 29,300 hrs · 24,128 cycles

WHILE PERFORMING REINSPECTION OF LT PRESSURE FLOOR SUPPORT BS 461 - 559, FOUND SEVERAL AREAS OF LIGHT CORROSION. BLENDED CORROSION IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,300 hrs · 24,128 cycles

LEFT FLAP VANE INBD CHAFED. R & R L/E CAP WITH NEW L/E CAP IAW REO AND SRM.

Part: PANEL — CRACKED (COCKPIT) · airframe 29,300 hrs · 24,128 cycles

PANEL 221BLC HAS CRACKS ON RIGHT CUTOUT FOR COCKPIT ESCAPE HATCH HINGE. REPAIRED PANEL 221BLC IAW STS EA.

Part: BATTERY PACK — FAILED (FLASHLIGHT) · airframe 29,124 hrs · 23,978 cycles

CABIN EMERGENCY FLASHLIGHT NOT WORKING. R & R F/A FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,949 hrs · 23,833 cycles

SIDEWALL EMERGENCY LIGHT AT 8A IS INOPERATIVE. REPLACED FWD EMERGENCY LIGHT IAW AMM.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 28,675 hrs · 23,583 cycles

LEFT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LT AFT EMERGENCY LIGHT BULB IAW AMM.

Part: LIGHT — DETACHED (CABIN) · airframe 28,650 hrs · 23,563 cycles

EMERGENCY FLOOR LIGHT STRIP HAS A PLASTIC PIECE THAT IS STICKING UP. RE-GLUED THE EMERGENCY LIGHT STRIP BACK INTO PLACE.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 28,002 hrs · 23,055 cycles

AFTER TAKEOFF SMOKE FILLED MORE THAN HALF COCKPIT. DONNED O2 MASK DECLARED EMERGENCY LANDED UNEVENTFULLY. SMOKE WAS FILLING AFT CABIN AS WELL, SMOKE CLEARED AFTER LANDING, RAN QRH. FLT 6331 PERFORMED OPERATIONAL TEST OF BOTH PACKS IAW AMM. NO SMOKE NOTICED IN COCKPIT & CABIN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,208 hrs · 22,397 cycles

POD 3 OVERHEAD EMERGENCY LIGHT BURNED OUT. FLT#4460 RELAMPED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 27,158 hrs · 22,351 cycles

GEAR DISAGREE WARNING MESSAGE. GEAR INDICATIONS SHOW NOSE GEAR DOWN & LOCKED, GEAR HANDLE IN UP POSITION. FLT#5368 READJUSTED NLG OLEO CENTERED EXTENDED PROXIMITY SENSOR IAW AMM. PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION RETRACTION SYSTEM. OPERATIONS CHECKED GOOD.

Part: PIN — SCORED (ENGINE MOUNT) · airframe 27,122 hrs · 22,322 cycles

RT ENGINE FORWARD MOUNT PINS SCORED. C-CHECK REPLACED THE RT FORWARD ENGINE MOUNT PINS.

Part: LINK — GALLED (ENGINE MOUNT) · airframe 27,122 hrs · 22,322 cycles

RT ENGINE YOKE LINK HAS GALLING. C-C-CHECK REPLACED RT ENGINE FORWARD MOUNT YOKE LINK ASSEMBLY.

Part: BEARING — GALLED (ENGINE MOUNT) · airframe 27,122 hrs · 22,322 cycles

LOWER BEARING ON RT ENGINE YOKE HAS GALLING. C-CHECK REPLACED RT ENGINE FORWARD YOKE MOUNT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,026 hrs · 22,243 cycles

OVERHEAD EMERGENCY LIGHT BURNED OUT. FLT#5505 RELAMPED.

Part: COVER — MISSING (CALL LIGHT) · airframe 26,994 hrs · 22,219 cycles

RED COVER MISSING ON FORWARD FACING MID CABIN FLIGHT ATTENDANT CALL LIGHT. FLT#5505 REPLACED RED COVER ON FORWARD FACING MID CABIN FLIGHT ATTENDANT CALL LIGHT.

Part: LENS — MISSING (EXIT SIGN) · airframe 26,865 hrs · 22,118 cycles

THE RED LENS ON THE EMERGENCY EXIT SIGN OVERHEAD IS MISSING. FLT#5319 REPLACED RED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,805 hrs · 22,066 cycles

EMERGENCY OVERHEAD LIGHT AFT OF EXIT SIGN IN CABIN IS BURNED OUT. FLT#5650 RELAMPED.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 26,639 hrs · 21,912 cycles

FLT 6318, STRONG FUEL ODOR THROUGH ALL PHASES OF FLIGHT. REPLACED BOTH WATER SEPARATOR COALESCERS IAW AMM. RAN APU & PACKS, NO FUEL ODOR NOTED. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,320 hrs · 21,676 cycles

EMERGENCY OVERHEAD LIGHT NEAR LAVATORY IS BURNED OUT. RELAMPED.

Part: BRACKET — FAILED (NLG) · airframe 26,082 hrs · 21,504 cycles

AFTER RAISING GEAR LEVER, RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE EMERGENCY MESSAGES. PERFORMED QRH AND ALL 3 WENT DOWN AND GREEN. (FLT 6491) REPLACED NLG OLEO CENTERING EXTENSION PROX SWITCH BRACKET IAW AMM. INSPECTED PROX SWITCH HARNESS AND FOUND NO DAMAGE AT THIS TIME. OPS CHECK GOOD. SWUNG THE GEAR SEVERAL TIMES AND PERFORMED EMERGENCY EXTENSION CHECK. ALL OPS CHECKS GOOD.

Part: BRACKET — BENT (NLG) · airframe 25,974 hrs · 21,417 cycles

GEAR DISAGREE, NOSE GEAR. (FLT 6496) STRAIGHTENED NLG WOW SENSOR BRACKET AND RE-INSPECTED THE GAP FOR NLG WOW SENSOR, IAW AMM. PERFORMED SEVERAL GEAR SWINGS IAW AMM. OPERATIONAL CHECK GOOD.

Part: COVER — MISSING (CABIN DOOR) · airframe 25,538 hrs · 21,031 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHT COVER MISSING. (FLT 4541) REPLACED FORWARD MAIN CABIN DOOR EMERGENCY EXIT LIGHT ASSEMBLY.

Part: SERVO — FAILED (ELEVATOR) · airframe 25,499 hrs · 20,997 cycles

UNCOMMANDED AP DISCONNECT IN TURNS AND DESCENT. ONCE AP KICKED OFF, THE YOKE WOULD JERK IN THE OPPOSITE DIRECTION OF THE TURN OR UP WHEN IN DESCENT. (FLT 7428) REPLACED ELEVATOR SERVO IAW AMM. P/N: 322-5027-001 S/N: 3018 S/N OFF: 142

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 25,492 hrs · 20,991 cycles

SMOKE CAUTION APPEARED AT ABOUT 10,000 FEET, THEN THE INDICATION WENT AWAY. (FLT 6441) RAN ENGINES AT TAKEOFF POWER WITH PACKS ON, NO SMOKE OR SMELL NOTED IN CABIN OR LAV. SUSPECT DEICE FLUID INGESTED IN PACK. OPS CHECKS GOOD AT THIS TIME.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 25,379 hrs · 20,892 cycles

RECEIVED SMOKE TOILET CAUTION MESSAGE. MESSAGE CLEARED, NO SMOKE OR FIRE OBSERVED. (FLT 1352) PERFORMED AN OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM IAW AMM. COULD NOT DUPLICATE FAULT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,057 hrs · 20,642 cycles

FS 621 BULKHEAD WEB HAS CRACK AT TOP OF LINTEL FITTING. (C-CHECK) REPAIRED FS 621 LINTEL IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 25,057 hrs · 20,642 cycles

VERTICAL POST AT FS 409.0 +128 RBL 18.0 OUTBOARD SIDE IS CRACKED. (C-CHECK) REPLACED VERTICAL POST AT FS 409.0 + 128 RBL 18.0 OUTBOARD IAW REO AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,316 hrs · 20,013 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6290) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,147 hrs · 19,881 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5557) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,085 hrs · 19,810 cycles

EMERGENCY EXIT SIGN HAS SEVERAL BULBS THAT ARE INOPERATIVE IN CENTER AISLE. (FLT 4727) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,031 hrs · 19,766 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 23,595 hrs · 19,369 cycles

FLOOR LEVEL EMERGENCY LIGHT AT MAIN CABIN DOOR IS INTERMITTENT. (FLT 6228) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,539 hrs · 19,323 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4227) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,526 hrs · 19,305 cycles

EMERGENCY EXIT SIGN AT MAIN CABIN DOOR LIGHTS ARE OUT. (FLT 6314) RE-RACKED NR 1 BATTERY PACK FOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,446 hrs · 19,243 cycles

FORWARD AND AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5415) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,405 hrs · 19,213 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6389) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,334 hrs · 19,153 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5590) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,028 hrs · 18,903 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4692) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,978 hrs · 18,850 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 5328) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,654 hrs · 18,552 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5362) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 22,464 hrs · 18,388 cycles

SIDEWALL EMERGENCY LIGHT BY MCD IS OUT. (FLT 6275) REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT BY MCD.

Part: LINK — CORRODED (ENGINE MOUNT) · airframe 22,166 hrs · 18,139 cycles

LEFT ENGINE YOKE LINK HAS GALLING INSIDE BUSHING. (ENGINE CHANGE) REPLACED LEFT ENGINE YOKE LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,020 hrs · 18,010 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,940 hrs · 17,941 cycles

THE 2ND FROM BACK OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 4474) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,915 hrs · 17,915 cycles

NR 3 RIGHT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,856 hrs · 17,861 cycles

RIGHT EXTERIOR MIDDLE OVERWING EMERGENCY LIGHT IS OUT. (FLT 4557) RELAMPED EMERGENCY LIGHT.

Part: CHARGER — FAILED (CABIN) · airframe 21,823 hrs · 17,831 cycles

CENTER EMERGENCY EXIT CEILING LIGHT IS OUT. (FLT 4537) REPLACED EMERGENCY BATTERY CHARGER NR 2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,823 hrs · 17,831 cycles

RIGHT OVERWING EXTERIOR MIDDLE EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 21,709 hrs · 17,738 cycles

GEAR DISAGREE MESSAGE. (FLT 5486) ADJUSTED NLG PROX SWITCH S23.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,212 hrs · 17,319 cycles

LEFT FLOOR SILL AT FS 449.85 LBL 44.5 IS CORRODED TO LIMITS. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,615 hrs · 17,669 cycles

FS 621 BULKHEAD, FORWARD FACE CRACKED AT UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,894 hrs · 17,059 cycles

NR 1 EMERGENCY CEILING LIGHT IS INOPERATIVE. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,791 hrs · 16,972 cycles

RIGHT WING EXTERIOR FORWARD EMERGENCY EXIT LIGHT IS OUT. (FLT 6487) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,404 hrs · 16,637 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6764) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,941 hrs · 16,251 cycles

CRACK INDICATION ON FS 559 PRESSURE BULKHEAD AT RIGHT SIDE, MARKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,094 hrs · 16,387 cycles

FS 559.0 PRESSURE BULKHEAD AT RT SIDE CRACKED. (C-CHECK) REPAIRED PER REO.

Part: ELEMENT — INTERMITTENT (NR 1 ENGINE) · airframe 18,805 hrs · 15,320 cycles

FLIGHT 5516, IAH TO ATL. THE FLIGHT CREW REPORTED AN ANTI-ICE DUCT FAIL MESSAGE ON EICAS, WITH WING ANTI-ICE DUCT FAIL ILLUMINATED ON THE PUSH BUTTON. THE SYNOPTIC PAGE ON EICAS SHOWS THE LEFT-HAND FUSELAGE DUCT IN RED. THE AIRCRAFT WAS NEVER IN ICING CONDITIONS AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 14TH STAGE SENSING LOOP TO BE BAD. THE LOOP WAS REPLACED AND THE SYSTEM OPERATED NORMALLY.

Part: CLAMP — LOOSE (14TH STAGE DUCT) · airframe 18,804 hrs · 15,318 cycles

FLIGHT 5531, SDF TO IAH. ON CLIMB OUT FROM SDF THE CREW RECEIVED L 10TH DUCT, ANTI ICE DUCT, AND L 14TH DUCT MESSAGES ON EICAS. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LOOSE CLAMP ON THE 14TH STAGE CHECK VALVE BETWEEN THE SHUT-OFF VALVE AND THE WING ANTI-ICE VALVE. THE CLAMP WAS RE-SECURED AND THE SYSTEM OPERATED NORMALLY.

Part: POWER CABLE — DEFECTIVE (CABIN) · airframe 18,248 hrs · 14,863 cycles

DURING INSPECTION THE FLOOR EMERGENCY LIGHTS NEAR ROW NR 1 WERE INOPERATIVE WHEN TESTED. THE LIGHT STRIP WAS SWAPPED WITH THE AFT STRIP AND THE FAULT FOLLOWED. THE LIGHT STRIP WAS LEFT IN THE AFT POSITION AND DEFERRED. THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT FLOOR POWER CABLE IAW AMM 33-51-01, OPS CHECK GOOD.

Part: CONTROL UNIT — FAULTED (STAB TRIM MOTOR)

FLIGHT 5338, IAH TO VPS. AFTER TAKEOFF THE CREW RECEIVED A STAB TRIM CHANNEL 1 FAIL MESSAGE AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND FAULT CODES POINTING TO THE MOTOR CONTROL UNIT. THE MOTOR CONTROL UNIT WAS REPLACED AND THE TRIM SYSTEM OPS CHECKED GOOD DURING THE TEST FLIGHT. (S)

Part: UNKNOWN — ODOR (CABIN) · airframe 13,497 hrs · 11,433 cycles

FLIGHT 3268 - DFW-CLE - IN CRUISE FLIGHT, FLIGHT ATTENDANT CALLED AND SAID THE BACK WAS COLD. TURNED UP THE RIGHT PACK. FLIGHT ATTENDANT CALLED BACK AND SAID IT WAS STILL COLD IN THE BACK; PULLED UP ECS PAGE AND TURNED THE PACK UP AGAIN AND MONITORED IT. ABOUT 5 MINUTES LATER, RECEIVED SMOKE TOILET INDICATION. THERE WAS NO FIRE OR SMOKE IN THE CABIN BUT SMELL WAS ABOUND. TURNED PACK BACK DOWN TO FULL COLD, RAN QRH, SMELL DISAPPEARED. FLIGHT ATTENDANT PULLED THE SAFETY PIN ON THE HALON BOTTLE AND WENT BACK, BUT THERE WAS NO FIRE AND THE SMELL WAS GONE. MAINTENANCE REMOVED AND REPLACED THE SEAL.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

STALL FAIL MESSAGE POSTED AFTER T/O. RESET STALL PROTECTION COMPUTER. NO FAULT CODES RECORDED IN COMPUTER.

Part: BATTERY — WEAK (EMERGENCY LIGHT)

FWD EMERGENCY LIGHTS INOP. REPLACED NR 1 EMERGENCY BATTERY.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

CREW REPORT STATES RECEIVED CAUTION MSG HYD PUMP 3B INOP. OHM WIRING FOR THE 3B HYD PUMP TO CIRCUIT BREAKER A2 ON CB PNL 1. NO DEFECTS ARE NOTED IN WIRING REPLACE 3B HYD PUMP. THIS WO IS STILL IN APPR STAGE.

Part: HANDLE — INOPERATIVE (PAX DOOR)

PASSENGER DOOR WILL NOT OPEN. CLEANED AND LUBED PASSENGER DOOR INNER HANDLE. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

RIGHT FWD EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR ON EMERGENCY BATTERY REF AMM 33-51-04. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT HAND NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,898 hrs · 6,519 cycles

DURING INSPECTION, THE CEILING EMERGENCY LIGHT 2ND FROM FROM WAS FOUND INOPERATIVE. MAINTNANCE PERSONNEL REMOVED AND REPLACED THE BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. THE AIRCRAFT WAS FERRIED TO IAD FOR MAINTENANCE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.