N606QX
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
248 reports on file, 2001-09-25 – 2011-02-17.
Part: STRINGER — CORRODED (BS 295-310) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP FOUND CORROSION ON STR 25R AT FS295-310. BEGAN CORROSION REMOVAL, FOUND STR TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A01. MADE REPAIR IAW REO 670-53-21-643.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP, FOUND CORROSION ON NLG JACK FITTING SUPPORT ANGLE ATTACH FLANGE. BLENDED SURFACE CORROSION IAW SRM 51-21-06-001-001-A01. DEEPEST BLEND ON FLANGES IS .003 MATERIAL REMOVED. ORIGINAL THICKNESS IS .063. PERFORMED FPI ON BLENDED AREAS OF NLG IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. SENT ENGINEERING REQUEST. RECEIVED REO 670-53-11-573. BLENDED AREA ACCEPTABLE IAW REO. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IAW TASK CARD REO 670-53-11-573.
Part: FLOOR SUPPORT — CORRODED (E/E BAY) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - SUPPORT ANGLE FOR AVIONICS BAY FLOOR PANEL 141 ALF CORRODED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. PERFORMED LPI TO ANGLE IAW NDTM 51-20-008-280-A01, NO DEFECTS , CRACKS NOTED. FABRICATED AND INSTALLED NEW ANGLE ALL WORK DONE IAW REO 670-53-11-576.
Part: DOUBLER — CORRODED (BS 333 S25R) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP FOUND CORROSION ON STR 25R SPLICE DOUBLER AT FS 333. REMOVED CORROSION ON 25R SPLICE DOUBLER, FOUND OUT OF LIMITS IAW SRM 53-21-03-101-002-A02. REPAIRED IN CONFORMANCE WITH TASK CARD REO 670-53-21-643.
Part: STRINGER — DAMAGED (BS 280-295) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - CORROSION FOUND ON FREE FLANGE OF STR 26R BETWEEN FS 280.00 - 295.00. BLENDED CORROSION, DAMAGE IN NO DAMAGE ALLOWED AREA IAW SRM 53-21-03-991-855. ALL BLENDS DONE IAW SRM 51-21-06-001-001-A01. PERFORMED FPI ON BLENDED AREAS IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. R & R STRINGER SECTION IAW REO 670-53-21-643.
Part: STRUCTURE — CORRODED (BS 280-310) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP, FOUND CORROSION ON STR 25L AT FS 280, FS 310. REMOVED ALL CORROSION AND FOUND FS 280-FS 295 TO BE IN NO DAMAGE ALLOWED AREA. PERFORMED FPI IAW NDTM 51-20-08, NO EVIDENCE OF CRACK FOUND. FABRICATED REPAIR PARTS IAW REO 670-53-21-643. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01 AND REO 670-53-21-643. INSTALLED REPAIR IAW REO 670-53-21-643. ALL WORK DONE IAW TASK CARD REO 670-53-21-643.
Part: STRINGER — CORRODED (BS 333 S25R) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - CORROSION FOUND ON STR 25R AT FS 333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A02. REPAIRED IN CONFORMANCE WITH TASK CARD REO 670-253-21-643.
Part: STRINGER — CORRODED (BS 300 S26L) · airframe 24,982 hrs · 18,568 cycles
RFD - C6 CHECK - CORROSION FOUND ON STR 26L AT FS 300. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDS WITHIN LIMITS IAW SRM 53-21-03-101-002-A01. PERFORMED FPI ON BLENDED AREAS IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. TREATED, PRIMED AND PAINTED AS REQUIRED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.
Part: ATTACH FITTING — CORRODED (BS 280-295) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP FOUND CORROSION ON STR 25R ATTACH FLANGE BETWEEN FS280-295. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CORROSION FOUND TO BE IN NO DAMAGE ALLOWED AREA IAW SRM 53-21-03-101-002-A01. REPAIRED IAW REO 670-53-21-643.
Part: BEAM — DAMAGED (FUSELAGE) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - FWD LINTEL BEAM ON AFT BAGGAGE BAY SURROUND IS CHAFED. REMOVED LINTEL BEAM AND DISASSEMBLED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. BLENDED DAMAGED AREA IAW SRM 51-12-00-001-001-A01. PERFORMED LPI OF AFFECTED AREAS, NO DEFECTS NOTED IAW NDTM 51-20-08-230-80. FABRICATED REPAIR ANGLES IAW REO 670-53-61-701. TREATED, PRIMED AND PAINTED REPAIR ANGLES IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED REPAIR ANGLES AND LINTEL BEAM IAW REO 670-53-61-701. TOPCOATED LINTEL BEAM IAW SRM 51-25-16-001-001-A01.
Part: BUTTSTRAP — CORRODED (BS 280) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - DURING INSP FOUND CORROSION ON FS 280 BUTTSTRAP BETWEEN STR 25L AND 26R. CORROSION FOUND TO BE LOCATED IN NO DAMAGE ALLOWED AREA IAW SRM 53-21-01-101-002-A01. SENT ENGINEERING REQUEST. PERFORMED FPI ON AREA IAW NDTM 51-20-008-230-A01. TREATED, PRIMED AND PAINTED AREA IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED COMPLIES WITH QX TASK CARD REO 670-53-21-652.
Part: STRUCTURE — CHAFED (RT SLATS) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SLAT 2 AND 3 HAVE EVIDENCE OF CHAFING AT WS 178, 178+70 AND 178+129, 178+138 AND WS 294. BLENDED AREAS IAW SRM 51-12-00-001-001-A01. PERFORMED FPI IAW SRM NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK DONE IAW TASK CARDS REO 670-57-42-286 AND REO 670-57-42-287.
Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - SERVICE DOOR SILL HAS SIGNS OF CORROSION. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BOTH STRIKER SEAL AND MOUNTING ANGLE WERE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED STRIKER SEAL AND MOUNTING ANGLE IAW SRM 51-42-06. INSTALLED NEW MOUNTING ANGLE AND STRIKER SEAL IAW SRM 51-42-06-001-001-A01 AND 51-42-02-001-001-A01. APPLIED TOPCOAT AND CORROSION PREVENTATIVE IAW 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - CORROSION FOUND IN PAX DOOR SILL AREA ON MID CAP ANGLE AND SUPPORTING STRUCTURE. REMOVED MID CAP ANGLE AND FOUND CORROSION PRESENT ON BOTH VERTICAL FLANGE AND OTBD CORNER RADIUS, OUT OF LIMITS IAW SRM 51-12-00-001-001-A01. REMOVED DOOR SILL MOUNTING ANGLE IAW SRM 51-40-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW DOOR SILL MOUNTING ANGLE AND NEW MID CAP ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01. PRIMED AND PAINTED AS NECESSARY THE DOOR SILL MOUNT ANGLE AND MID CAP ANGLE IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.
Part: FLOORBEAM — DAMAGED (BS 280) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - FS 280 CROSSBEAM RIDING ON, WORKING AGAINST LONGITUDINAL FLOORBEAM CAPS AT RBL 11 AND LBL 11. REMOVED AND INSTALLED NEW 280, WORKED FLOORBEAM LONGITUDINAL CAPS AND COMPLETED REPAIR IAW REO 670-53-11-045, 670-53-11-047, NDTM 51-20-08 AND SRM 51-25-06-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
Part: STRUCTURE — CHAFED (NR 2 SLAT) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SLAT NR 2 HAS EVIDENCE OF CHAFING AT WS 178, 178+21, 178+70 AND 178+138 OTBD END APPROX LAST 15" OF SLAT. REPAIRED IAW REO 670-57-42-285.
Part: PANEL — CHAFED (RT WING) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SLAT LOWER T/E IS CHAFED INTO PANEL 622CB. BLENDED CHAFE DAMAGE, PERFORMED FPI ON AREA IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. SENT ENGINEERING REQUEST TO MFG. RECEIVED ENGINEERING REO 670-57-42-288, AREA IS OK AS BLENDED. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.
Part: FASTENER — LOOSE (SPOILER) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - SEVERAL LOOSE/MISSING FASTENERS IN WING T/E JUST OTBD OF RT MULTIFUNCTION SPOILER. REMOVED LOOSE RIVETS AND INSTALLED NEW RIVETS IAW SRM 51-42-06-001-001-A01. PREPPED, PRIMED AND PAINTED IAW SRM 51-25-01.
Part: BULKHEAD — CORRODED (BS 280) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT FS 280 LOWER BULKHEAD HAS CORROSION AT OTBD SECTION OF WEB. BLENDED CORROSION IAW SRM 53-11-10-201-003-A01 AND 51-26-06-001-001-A01. BLEND FOUND TO BE WITHIN LIMITS IAW SRM 53-11-10-201-003-A01. ETCHED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01. ALL WORK IAW SRM TASK 53-11-10-201-003-A01.
Part: ANGLE — CORRODED (ZONE 100) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - ANGLE AT FS 280 CTR SECTION CORRODED THROUGHOUT ENTIRE LENGTH. REMOVED CORRODED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. RESTORED SURFACE IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.
Part: GUSSET — CRACKED (ZONE 100) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - GUSSETT CRACKED ON RT FS 280 FLOORBOARD SUPPORT. REMOVED CRACKED GUSSETT IAW SRM 51-42-06-001-001-A01. PREPARED NEW AND INSTALLED NEW GUSSETT IAW SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 714-761) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDE SEAT RAIL FROM FS 714-761 HAS CORROSION. REMOVED CORROSION FOUND TO BE IN COUNTERSINKS AND BEYOND LIMITS IAW 53-31-49-101-001-A01. REMOVED DAMAGED SEAT TRACK, PREPARED NEW TRACK IAW SRM 51-40-11-001-001-A01 AND 51-21-11-001-001-A01 AND INSTALLED NEW RT SIDE SEAT TRACKS IAW AMM 53-00-49-400-801-A01.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 23,982 hrs · 18,568 cycles
C6 CHECK - CRACK DISCOVERED IN FWD EQUIPMENT COMPARTMENT ON WL 79.5 FLOOR UNDER ADG PUMP. REPAIRED IAW REO 670-53-11-0509.
Part: FLOOR PANEL — CRACKED (BS 193) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - CRACK FOUND ON LT SIDE OF FWD EQUIPMENT COMPARTMENT AT FS 193 IN ELECTRIC BAY FLOOR SKIN LT SIDE. CUT AWAY DAMAGE/ FABRICATED PARTS IAW REO 670-53-11-509. PREPARED AREA OF CUTOUT FOR NDT IAW SRM 51-26-00-001-001-A01. PERFORMED FPI ON SKIN AROUND CUTOUT APPROX .500" AROUND CUTOUT SECTION IAW NDTM 51-20-08, NO EVIDENCE OF CRACK FOUND. INSTALLED FABRICATED PARTS IAW REO 670-53-11-509.
Part: PLATE — CORRODED (CARGO BAY) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - FWD BAGGAGE BAY DOOR FWD JOINT PLATE IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .009 IN ANY ONE AREA. PERFORMED FPI IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS. ENGINEERING REQUEST SENT, RECEIVED ENGINEERING REO 670-53-31-195, AREA IS ACCEPTABLE AS IS. RESTORED FINISH AMM 51-25-16-001-001.
Part: SILL — CHAFED (CARGO DOORWAY) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - AFT BAGGAGE DOOR SILL IS CHAFED AND SHOW SIGNS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-11-001-001-A01. MAPPED AND SENT ENGINEERING REQUEST TO MFG. PERFORMED FPI ON BLENDED AREAS OF AFT BAGGAGE DOOR SILL IAW NDTM 51-20-08 IAW REO 670-53-61-696, NO EVIDENCE OF CRACKS FOUND. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01. ALL PREVIOUS WORK DONE IAW REO 670-53-61-696.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - CRACK ON LOWER CHANNEL OF AFT CARGO DOOR TRACK. REMOVED CRACKED LOWER CHANNEL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW LOWER CHANNEL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 484-574) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL SEGMENT FROM FS 484-574 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .008", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 574-664) · airframe 23,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL SEGMENT FROM FS 574-664 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .009", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 840-866) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL FROM FS 840-866 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .009". REMOVED MATERIAL IN LIMITS IAW SRM 53-51-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 379-458) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL FROM FS 379-458 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .010", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 458-484) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDE SEAT RAIL FROM FS 458-484 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .007", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 486-582) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT AISLE SEAT TRACK FROM FS 486-582 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. BLENDED OUT ALL CORROSION MAX MATERIAL REMOVED .010" D, .050" W AND 20" L. REMAINING MATERIAL THICKNESS .115". FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 785-840) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDE SEAT RAILS FROM FS 785-840 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .007" FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01.
Part: SEAT TRACK — CORRODED (BS 458-484) · airframe 23,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL FROM FS 458-484 HAS CORROSION PRESENT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .012", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT AISLE SEAT TRACK FROM FS 379-477 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. MAX MATERIAL REMOVED .018" D, .500" W AND 7" L. REMAINING MATERIAL THICKNESS .356" IAW SRM 51-21-01-001-A01. CORROSION FOUND TO BE WITHIN LIMITS. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 582-664) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT AISLE SEAT TRACK FROM FS 582-664 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. BLENDED OUT ALL CORROSION .020" D, .050" W AND 48" L. REMAINING MATERIAL THICKNESS .355". FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 574-664) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDEWALL SEAT RAIL FROM FS 574-664 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .007", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SILL — DAMAGED (BS 953-969) · airframe 24,982 hrs · 18,568 cycles
DIAPHRAGM IN FLOOR SILL BETWEEN FS 953-969 LT, DAMAGED. REMOVED DIAPHRAGM REF AMM 20-21-00-910-801-A01 AND SRM 51-42-06-001-001-A01 AND INSTALLED NEW DIAPHRAGM REF AMM 20-21-00-910-801-A01 AND SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 664-693) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT AISLE SEAT TRACK FROM FS 664-693 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MATERIAL REMOVED .008" DEEP, .500" WIDE AND 20' LONG, REMAINING MATERIAL THICKNESS .367. FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 714-761) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL FROM FS 714-761 HAS SOME AREAS OF CORROSION. REMOVED CORROSION IN SEVERAL AREAS IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .005" AT ANY ONE LOCATION, FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 484-574) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDEWALL SEAT RAIL FROM FS 484-574 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .008", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 676-714) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT SIDE SEAT RAIL FROM FS 676-714 HAS SOME AREAS OF CORROSION. REMOVED CORROSION IN SEVERAL AREAS IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .006" AT ANY ONE LOCATION, FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 379-458) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDE SEAT RAIL FROM FS 379-458 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .009", FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 664-693) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT AISLE SEAT TRACK FROM FS 664-693 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MATERIAL REMOVED NO MORE THAN .008" REMAINING MATERIAL THICKNESS .295". FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 676-714) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - RT SIDE SEAT RAIL FROM FS 676-714 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED NO MORE THAN .008", FOUND IN LIMITS IAW SRM 53-51-49-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 383-486) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT AISLE SEAT TRACK FROM FS 383-486 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. MAX MATERIAL REMOVED .008" D, .500" W AND 16" L. REMAINING MATERIAL THICKNESS .367". FOUND TO BE WITHIN LIMITS IAW SRM 51-21-01-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: STRUCTURE — DAMAGED (SPOILER) · airframe 24,982 hrs · 18,568 cycles
SEVERAL WORKING, MISSING FASTENERS WING T/E JUST OTBD OF LT MULTIFUNCTION SPOILER. REMOVED WORKING, MISSING FASTENERS IAW SRM 51-42-06-001-001-A01 AND INSTALLED NEW FASTENERS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01 AND 51-12-00-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 486-582) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT AISLE SEAT TRACK FROM FS 486-582 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. MAX MATERIAL REMOVED .010" D, .500" W AND 31" L. REMAINING MATERIAL THICKNESS .365". FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 582-664) · airframe 24,982 hrs · 18,568 cycles
C6 CHECK - LT AISLE SEAT TRACK FROM FS 582-664 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-A01. BLENDED OUT ALL CORROSION MAX MATERIAL REMOVED .025" D, .500" W AND 23" L. REMAINING MATERIAL THICKNESS .350". FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-A01 AND REO 670-53-00-013.
Earlier reports · 2001–2010 · 198 reports
2010
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 24,664 hrs · 18,333 cycles
DURING THE LINE CHECK 1 FOUND THE RT OVERWING EMERGENCY EXIT DOOR LIGHT TO BE INOPERATIVE. REPLACED THE EPSU BATTERY PACK IAW TASK 33-51-17-000-801.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,295 hrs · 18,039 cycles
CLIMBING THROUGH 25,500 WITH SPEED AT 290 KTS. SELECTED, THE SELECTED SPEED ROLLED BACK TO 270K. RETURNED TO THE FIELD, LANDING UNEVENTFUL. COMPLIED WITH SL REV E. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.
Part: REGULATOR VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 24,126 hrs · 17,910 cycles
ON TAXI OUT, ODOR OF SMOKE NOTICED. RETURNED TO THE GATE. REPLACED NR 2 ENGINE SEAL PRESSURE REGULATOR VALVE OP CHECK GOOD NO ODOR OF SMOKE. RETURNED TO SERVICE.
2009
Part: ANGLE — CRACKED (CARGO DOOR) · airframe 21,021 hrs · 15,582 cycles
PDX - MOD - MCD AFT CLOSING ANGLE IS CRACKED AT PULLET BRACKET. REMOVED PANEL 832DR AND MCD PULLEY BRACKET TO FOM REMOVAL OF CLOSING ANGLE. REMOVED PREVIOUS REPAIR FROM MAIN CABIN DOOR. TRIMMED NEW SPLICE ANGLE FROM 601R31772-5 TO LENGTH AND BEGAIN TO TRANSFER HOLES NOTE 13 REO670-52-11-072. FABRICATED NEW -3 SPLICE ANGLE AND MATCH DRILLED TO A/C COMPLETED DRILLING UP -1 ANGLE SECTION PER REO670-52-11-072. ALODINE, PRIME, AND PAINTED -3 SPLICE IAW REO670-52-11-072 NOTE 10. INSTALLED REPAIR ANGLES AS PER REO 670-52-11-072 AND REO670-52-11-439. INSTALLED TWO NUTPLATES IN REPAIR ANGLE IAW CRJ 700 SRM 51-42-06, EDGE SEALED REPAIR ANGLE AND MCD PULLEY BRACKET IAW REO670-52-11-072 AND APPLIED TOP COAT TO REPAIR AND FASTENERS IAW REO 670-52-11-072. INSTALLED PANEL 832DR .
Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,021 hrs · 15,582 cycles
PDX - MOD - EXTERIOR SKIN IS CHAFED 1 INCH LONG WITH DENT ADJACENT TO IT AT FS 980 AND 6 O`CLOCK, CAUSED BY CONTACT WITH PANELS 195DL AND 196DR. BLENDED SMALL CHAFE MARK TO REMOVE DAMAGE FROM SCREW CONTACTING SKIN. FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-61-01-101-003-A01 DUE TO DENTED AREA. CHAFED AREA IS STILL DAMAGED ALONG THE FASTENER LINE. HFEC INSPECTED DENT AND CHAFED AREA FOR CRACKS IAW CRJ 700 NDTM PT 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK OF CHAFE AND DENT AREA IAW CRJ 700 NDTM PT 1, 51-20-004. CHAFE HIGH; .112 LOW; .109. DENT HIGH; .106 LOW; .064. BLENDED REMAINING DAMAGE ALONG FASTENER LINE. HFEC INSPECTED BLENDED AREA FOR CHAFE IAW CRJ 700 NDTM PT 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW CRJ 700 NDTM PART1, 51-20-04. HIGH .112 LOW .069. REMOVED THREE HI LITES IN AREA OF BLEND, MAPPED FOR ENGINEERING. REMOVED FASTENERS AND CUT OUT DAMAGE IAW REO670-53-61-498/3. HFEC IAW CRJ700 NDTM PT 1, 51-20-006 AT CUTOUT, NO CRACKS NOTED. FABRICATED NEW DOUBLERS AND FILLERS IAW REO 670-53-61-498/3. FABRICATED SHIMS, APPLIED ETCH AND ALODINE AND PRIMER TO ALL PIECES IAW REO670-53-61-498/3 NOTES 3, 6-8,11 AND 17. INSTALLED REPAIR IAW REO670-53-61-498/3 WITH FILLER, DOUBLERS AND SHIM. FILLET SEALED DOUBLER, PRIMED AND PAINTED AREA.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 21,021 hrs · 15,582 cycles
PDX - MOD LOWER BULKHEAD WEB AT FS 280 LT HAS AREAS OF CORROSION. BLENDED OUT CORROSION IAW CRJ REO 670-53-11-052. UT THICKNESS CHECKED AT BLENDED AREA IAW CRJ 700 NDTM PART 1, 51-20-004 AND FOUND HIGH READING .040" AND LOW .030". LT BULKHEAD WEB FOUND TO BE OUT OF LIMITS IAW CRJ REO 670-53-11-052. REMOVED FASTENERS IN WEB AND FASTENERS NECESSARY FOR ACCESS IAW CRJ SRM 51-42-06. NEW WEB DRILLED UP AND DEBURRED REF REO 670-53-11-052. INSTALLED NEW WEB REF REO 670-53-11-052. INSTALLED WIRE BUNDLES TO STANDOFFS.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 21,021 hrs · 15,582 cycles
PDX - MOD - SUSPECTED CRACK 1.5 INCHES LONG ON STR 3L EXTENDING FORE AND AFT FROM STA 280.0 TO STA 282.0. HFEC INSPECTED SUSPECTED CRACK IAW CRJ 700 NDTM PT 6 53-00-000-250-A01. CONFIRMED CRACK 1.5 INCHES LONG. MAPPED FOR ENGINEERING. CUT AWAY CRACK REMOVED FASTENERS FROM REPAIR AREA IAW TC REO670-53-21-480/1. HFEC INSPECTED CUTOUT FOR CRACKS IAW CRJ 700 NDTM PT 6, 53-00-000-250-A01. NO CRACKS NOTED. FABRICATED DOUBLER AND SHIMS, LOCATED AND DRILLED IAW TC REO 670-53-21-480/1. APPLIED FINISH TO REPAIR PARTS PER CRJ SRM 51-21-16. INSTALLED THE REPAIR, PRIMED AND TOP COATED IAW TC REO670-53-21-480/1.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 21,021 hrs · 15,582 cycles
LEFT INBD SEAT TRACK LOCATED BETWEEN FS 485 AND FS 581 IS CORRODED IN MULTIPLE AREAS. BLENDED OUT CORROSION IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED BLENDED AREA AND FOUND LESS THAN .013" MATERIAL REMOVED. REMAINING MATERIAL IS .097" TRACK WITHIN LIMITS IAW REO 670-53-00-013. ALODINED AND IDENTIFIED REPAIRS AT 485-581 IAW REO 670-53-00-013.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,021 hrs · 15,582 cycles
BS 280 FLOORBEAM IS CORRODED ON TOP OF AFT FLANGE FROM APPROX RBL 12 TO LBL 28. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AFT AND FWD DOUBLER AS PER REO 670-53-11-047. REMOVED FLOORBEAM AND INTERCOSTAL. CLEANED PRIMED AND PAINTED LOWER WEB NO CORROSION NOTED IAW CRJ 700 SRM 51-25-00. LOCATED AND DRILLED NEW FLOORBEAM DEBURRED REF REO 670-53-11-047. COMPLETED INSTALLATION IAW REO 670-53-11-052.
Part: SEAT TRACK — CORRODED (BS 379) · airframe 21,021 hrs · 15,582 cycles
AN AREA OF LIGHT CORROSION ON THE LT INBD SEAT TRACK AT FS 379.0 AND TOP OF THE TRACK. REMOVED CORROSION IAW REO 670-53-00-013 NOTES 1 AND 2. MEASURED BLENDED AREA AND FOUND NO MORE THAT .010" MATERIAL REMOVED, REMAINING THICKNESS IS .490 TRACK WITHIN LIMITS IAW REO 670-53-00-013. ALODINED AND IDENTIFIED REPAIRS AT 379.0 IAW 670-53-00-013
Part: ANGLE — CRACKED (BS 280) · airframe 21,021 hrs · 15,582 cycles
FWD SIDE OF BULKHEAD 280 BL 26 ANGLE CRACKED. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE IAW SRM 53-11-10 INSTALLED IAW SRM 51-42-06.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,021 hrs · 15,582 cycles
PDX - MOD - THERE IS CORROSION ON AND AROUND THE THREE RIVETS ON STRINGER 18L AT FS 549.00. REMOVED RIVETS FROM BRACKET AND FOUND EXCESSIVE CORROSION UNDER THE RIVET HEADS. REMOVED REMAINING RIVETS AND REMOVED CLEAT FROM STR 18 AT FS 549.00. FABRICATED NEW CLEAT OUT OF 2024-T3 .063 ALUMINUM ALLOY AS PER CRJ 700 SRM 53-31-23 PG 26 ITEM 109 AND QX GPM 5.12.4. INSTALLED CLEAT IAW CRJ SRM 51-42-00 AND 51-42-13 AND PRIME AREA IAW SRM 51-25-06.
Part: SEAT TRACK — CORRODED (BS 847-1031) · airframe 21,021 hrs · 15,582 cycles
LEFT INBD SEAT TRACK LOCATED BETWEEN FS 847 AND FS 1031 IS CORRODED IN MULTIPLE AREAS. REMOVED CORROSION FROM AFFECTED AREAS OF LT INBD SEAT TRACK BETWEEN FS 847 AND 1031 BY BLENDING IAW REO 670-53-00-013 NOTES 1,4 AND 6-7. MAX DEPTH AT DIMENSION "U" IS .014" AND MAX DEPTH AT DEMENSION "T" IS .024. BLEND IS WITHIN LIMITS AS PER REO 670-53-00-013. ALODINED SEAT TRACK (LT INBD) IN MULTIPLE AREAS BETWEEN FS 847 AND FS 1031 REF SRM 51-21-11.
Part: AXLE — DAMAGED (MLG) · airframe 20,819 hrs · 15,425 cycles
PDX - RIGHT AFTER INITIAL BREAK APPLICATION DURING LANDING THERE WAS A SEVERE SHAKING FOLLOWED BY A WOW INPUT CAUTION MESSAGE AND A PROX SYS FAULT 1 STATUS MESSAGE, BRAKE TEMP AFTER PARKING WERE 1-4, 2-4,3-1, 4-1 THE TOWER REPORTED SEEING SMOKE EMANATING FROM THE RIGHT MAIN WHEEL AREA. PERFORMED EXTENSIVE GEAR INSPECTION AND AIRFRAME INSPECTION, REMOVED AND REPLACED LOWER PISTON/AXLE ASSY, UPPER AND LOWER TQ LINKS, NR 3 AND NR 4 BRAKED AND TIRES AND SHIMMY DAMPER, REFERENCE REO 670-32-11-320 FOR DISPOSITION AND APPROVAL OF RETURN TO SERVICE, ALL FUNCTIONAL CHECKS GOOD.
2008
Part: BRAKE — DRAGGING (MLG) · airframe 17,275 hrs · 12,586 cycles
PDX - FLIGHT 2578 - AIRCRAFT PULLS TO THE LEFT DURING LANDING ROLL AND TAXI. BASED ON THE BRAKE TEMP INDICATIONS, SUSPECT THE LEFT OUTBOARD BRAKE IS DRAGGING. MAINTENANCE JACKED THE LT WHEELS AND CHECKED ROTATION WITH NO DEFECTS NOTED. COMPLIED WITH RIGGING CHECK OF THE RDVT AND RAN AUTO RIG WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
2007
Part: WIRE HARNESS — MALFUNCTIONED (WOW) · airframe 17,126 hrs · 12,490 cycles
PDX - FLIGHT 2612, RECEIVED A BRAKE OVERTEMP WARNING AFTER TAKEOFF. RETURNED TO THE FIELD. CFR CALLED AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT CURRENTLY OUT OF SERVICE FOR REPAIRS. MAINTENANCE REPLACED THE RIGHT MAIN GEAR OUTBOARD WOW HARNESS. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — BROKEN (TEMP SENSOR) · airframe 17,117 hrs · 12,482 cycles
SEA- FLIGHT 2631 - BRAKE OVERHEAT WARNING ON APPROACH BEFORE GEAR DOWN SELECTION. BTMS IN RED READS 00 UNITS. NO AURAL MESSAGE. PER THE CHECKLIST PRESSES THE RESET AND THE WARNING WENT NORMAL GREEN. MAINTENANCE FOUND THE TEMP SENSOR CONNECTOR BROKE INTERNALLY FOR THE RIGHT OUTBOARD SENSOR. PERFORMED REO 670-32-46-001. CAPPED AND STOWED THE CONNECTOR AND PLACED ON MEL 32-46-1. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING MESSAGE — ILLUMINATED · airframe 17,024 hrs · 12,412 cycles
FLIGHT 2621, ON TAXI RECEIVED A AFT CARGO SOV MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 21-55-4A. AIRCRAFT RETURNED TO SERVICE.
Part: ACM — SMOKE (RIGHT) · airframe 16,744 hrs · 12,233 cycles
SMF - FLIGHT 2576, AT THE GATE DURING ENGINE START, RECEIVED SMOKE IN THE CABIN AND A RIGHT AC PACK FAIL MESSAGE. REMOVED THE PASSENGERS FROM THE PLANE WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT PACK ON MEL 21-51-1B. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE AND THE RIGHT PACK DISCHARGE SENSOR. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 16,328 hrs · 11,956 cycles
PDX - CREW REPORTS FUEL DRIPPING FROM THE NR 2 ENGINE COWLING. MAINTENANCE REPLACED THE SLAVE COMPRESSOR VG ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — SHORTED (ANTI SKID SYS) · airframe 16,301 hrs · 11,936 cycles
PDX - FLIGHT 2352- AFTER PUSH BACK RECEIVED A ANTI-SKID CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND GROUNDING SHORT INSIDE CONNECTOR FOR NR 1 WHEEL SPEED TRANSDUCER. REPINNED PLUG AND GROUND SHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: TRANSDUCER — MALFUNCTIONED (WHEEL SPEED) · airframe 16,301 hrs · 11,936 cycles
PDX - FLIGHT 2290 - ON TAXI, RECEIVED A ANTI-SKID OUTBOARD CAUTION MESSAGE AND A SPOILER STAB FAULT. RETURNED TO THE GATE. MAINTENANCE FOUND THE BACKSHELL OF THE NR 1 WHEEL SPEED TRANSDUCER NOT ENGAGED. RESECURED AND RESET SSCU'S. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: COMPUTER — FAILED (STALL WARNING) · airframe 15,752 hrs · 11,569 cycles
PDX - FLIGHT 2560, STALL FAIL CAUTION MESSAGE AS WELL AS RIGHT AND LEFT FADEC MESSAGES IN CRUISE. PERFORMED CHECKLIST AND CAPTAIN'S STALL SWITCH STILL LEFT OFF. MAINTENANCE REPLACED THE STALL PROTECTION COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SHUTOFF VALVE — MALFUNCTIONED (A/C PACK) · airframe 15,587 hrs · 11,459 cycles
DEN - FLIGHT 4339, ON LIFT OFF, A RIGHT PACK TEMPERATURE CAUTION MESSAGE WAS RECEIVED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE HOT AIR SHUT OFF VALVE. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN (FIRE WARNING) · airframe 15,563 hrs · 11,440 cycles
BOI- FLIGHT 4276. FIRE SYSTEM FAULT ILLUMINATED. GOES OUT AFTER NR 1 ENGINE START. MAINTENANCE PLACED THE FIDEEX SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING MESSAGE — ILLUMINATED · airframe 15,400 hrs · 11,336 cycles
SEA - FIRE SYSTEM FAULT MESSAGE. PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE.
Part: SUPPORT ANGLE — CRACKED (NR 2 NACELLE) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - 2 ENGINE TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM END LATCH IS CRACKED. REPAIRED IAW REO670-78-800, AND SRM 51-42-13.
Part: SUPPORT ANGLE — CRACKED (THRUST REVERSER) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - NR 1 ENGINE LOWER TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM END LATCH IS CRACKED. REPAIRED IAW REO670-78-800, AND SRM 51-42-13.
Part: SKIN — GOUGED (R1 DOOR) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - RIGHT FORWARD SERVICE DOOR, R1, AFT LOWER CORNER OUTER SKIN HAS SMALL GOUGE. REPAIRED IAW SRM 52-41-00, 51-12-00, AND 52-41-01.
Part: SKIN — GOUGED (TE FLAP) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - LEFT WING, INBOARD FLAP, MIDDLE INBOARD VANE SPRING ACTUATOR AREA HAS A GOUGE IN THE SKIN. REPAIRED IAW SRM 51-12-00, 57-52-01.
Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - LEFT WING NR 3 SLAT 10.25" FROM OUTBOARD LEADING EDGE HAS ONE DEEP SCRATCH. REPAIRED IAW SRM 51-12-00, 57-42-01.
Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - NR 1 ENGINE UPPER TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM LATCH IS CRACKED. REPAIRED IAW REO670-78-33-800, AND SRM 51-42-13, 51-42-21.
Part: SKIN — CORRODED (FUSELAGE) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - LOWER ADF ANTENNA MOUNTING SKIN HAS LIGHT CORROSION. REPAIRED IAW SRM 51-21-06, AND 53-00-01.
Part: SKIN — CHAFED (RT TE FLAP) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - RIGHT FLAP PANEL 684AB CHAFED. REPAIRED IAW SRM 51-12-00, 51-21-11.
Part: SUPPORT — WORN (TE FLAP) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - RIGHT WING, OUTBOARD FLAPS, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-01, 51-12-00.
Part: SKIN — GOUGED (WING) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - PANEL 671AB GOUGED ON OUTER SURFACE. REPAIRED IAW SRM 57-31-01, 57-32-32.
Part: SUPPORT — WORN (LT WING) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - LEFT WING, OUTBOARD FLAP, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-02, 51-12-00.
Part: SKIN — DAMAGED (TE FLAP) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - PANEL 684ET HAS WEAR MARK ON LEADING EDGE. REPAIRED IAW SRM 55-00-00, 51-12-00.
Part: PANEL — CHAFED (WING) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - PANEL 584ET CHAFED AT LEADING EDGE. REPAIRED IAW SRM 53-00-01, 51-12-00, AND 53-00-01.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - PASSENGER CABIN LEFT SIDE SEAT RAIL FROM FS 485.00 LEFT TO FS 565.00 LEFT HAS NUMEROUS AREAS OF CORROSION AND SCRATCHES. REPAIRED IAW SRM 51-21-06 AND 51-21-11.
Part: SKIN — CORRODED (FUSELAGE) · airframe 15,333 hrs · 11,292 cycles
C4 OKC - LOWER FUSELAGE SKIN HAS MINOR CORROSION AT LOWER TCAS ANTENNA MOUNT. REPAIRED IAW SRM 51-21-06, 53-21-01.
Part: ROLLER — LACK OF LUBE (SERVICE DOOR) · airframe 15,204 hrs · 11,210 cycles
DEN - FLIGHT 4327- GALLEY SERVICE DOOR HARD TO UNLOCK AND OPEN. MAINTENANCE LUBED THE GALLEY DOOR ROLLERS AND HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: TIMER — MALFUNCTIONED (LAVATORY) · airframe 15,171 hrs · 11,185 cycles
DEN - FLIGHT 4277 - ON TAXI LAVATORY RUNS ALL THE TIME AND IS LEAKING FLUID. RETURNED TO THE GATE. MAINTNEANCE REPLACED THE GASKETS AND TIMER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN (ANTI ICE SYS) · airframe 15,148 hrs · 11,172 cycles
DEN - FLIGHT 4203, ON TAXI RECEIVED A "ANTI-ICE DUCT" WARNING. RETURNED TO THE GATE. MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND PERFORMED A ENGINE RUN WITH ANTI-ICE OPERATING. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 14,955 hrs · 11,039 cycles
SEA - AFTER TAKEOFF FOR FLIGHT 2542, FIRST OFFICER'S MULTI FUNCTION DISPLAY WENT BLANK. RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DISPLAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
2006
Part: DOOR — OPEN (CARGO BAY) · airframe 13,941 hrs · 10,362 cycles
SJC - FLIGHT 2502, UNABLE TO PRESSURIZE CABIN IN AUTO OR MANUAL MODE AFTER DEPARTURE FROM SJC. DIVERTED TO SMF AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE AFT CARGO DOOR NOT CLOSED PROPERLY. CHECKED THE DOOR, NO DEFECTS FOUND. DOOR OPERATES NORMALLY. OPERATIONAL CHECK OF PRESSURIZATION GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,537 hrs · 10,092 cycles
PDX - UPPER CENTER OF CAPTAIN'S WINDSHIELD APPEARS TO BE CRACKED. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD IAW AMM 56-11-01-00-801-A01 AND 56-11-01-400-801-A01. OPERATIONAL TEST OF TEMPERATURE CONTROLLER AND LEAK CHECK OF WINDOW ARE ALL GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 13,316 hrs · 9,933 cycles
SEA - FLIGHT 2380, RECEIVED A LEFT PACK FAULT MESSAGE ON PUSHBACK. RETURNED TO THE GATE. MAINTENANCE PLACE THE LEFT AC PACK ON MEL 21-51-4A. AIRCRAFT RETURNED TO SERVICE.
Part: STATUS MESSAGE — PILOT ERROR · airframe 13,120 hrs · 9,779 cycles
DEN - ON PUSHBACK FOR FLIGHT 4436 RECEIVED A APU FAULT STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE INTERROGATED THE MDC AND FOUND A UNDERSPEED MESSAGE POSTED. UPON INVESTIGATION FOUND POWER/FUEL BUTTON DESELECTED AND START/STOP BUTTON SELECTED. DESELECTED START/STOP BUTTON. FAULT MESSAGES CLEARED. OPERATIONAL CHECK OF THE APU IS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 12,121 hrs · 9,054 cycles
PDX - FLIGHT 2525 - YD 1 INOP STATUS MESSAGE. RETURNED TO THE GATE. DEFERRED IAW MEL REF 22-22-1 PLACARD NR 355850, AIRCRAFT RETURNED TO SERVICE. REPLACED THE YAW DAMPER LINEAR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WIRE — LOOSE (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE GENERATOR WIRING JUNCTION AT STATION 520, RIGHT BETWEEN STRINGER 2 AND 3 HAS ONE LOOSE TERMINAL AND ONE WIRE CONNECTOR HAS BURNED INSULATOR. REPAIRED IAW CRJ700 SRM 24-22-00-01-A01 AND AMM 24-22-01-710-801.
Part: CYLINDER — CORRODED (NLG) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 NOSE LANDING GEAR CORROSION ON OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-197 AND REO 670-32-21-083 SCR 0001-06 REV NC.
Part: LANDING GEAR — UNKNOWN (NOSE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 NOSE LANDING GEAR NEEDS REPAIR. REPAIRED IAW CRJ700 AMM TASK 32-21-22-400-801-A01, PARAGRAPH 2 (A-E)(10) AND AMM TASK 32-51-00-710-801.
Part: SKIN — NICKED (BS 1000) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR HAS NICKS ON SKIN ABOVE AFT BAGGAGE DOOR FUSELAGE STATION 1000 TO FUSELAGE STATION 1047, STRINGER 10R TO 12L. REPAIRED IAW HORIZON AIR EA R-53-422 AND CRJ700 SRM 51-25-01-001-001-A01.
Part: SKIN — CHIPPED (LT WING TE FLAP) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT WING INBOARD FLAP NUMEROUS ROCK CHIPS INPAINT AFT OF MAIN LANDING GEAR AREA. REPAIRED IAW CRJ700 SRM 51-21-26-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: DOOR FRAME — GOUGED (BS 319) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE GALLEY SERVICE DOOR SURROUND, FORWARD FRAME AT FUSELAGE STATION 319.70 HAS GOUGE 2" UP FROM FLOOR. REPAIRED IAW REO 670-53-21-159, REV A, HORIZON AIR EA R-53-425.
Part: SKIN — NICKED (BS 310-349) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR FUSELAGE STATION 310 TO 349, STRINGER 26L TO 25R, SKIN NICKED, GOUGED. REPAIRED IAW REO 670-53-21-162, HORIZON AIR EA R-53-429 AND CRJ 700/900 SRM 51-25-01-001-001-A01.
Part: SKIN — GOUGED (BS 331) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR FUSELAGE STATION 331 RIGHT ABOVE STRINGER 20R SKIN GOUGED. REPAIRED IAW REO 670-53-21-162, HORIZON AIR EA R-53-429 AND CRJ700/900 SRM 51-25-01-001-001-A01.
Part: SKIN — DAMAGED (BS 1051) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR HAS TWO AREAS OF NICKS ON SKIN AFT OF AFT BAGGAGE DOOR FUSELAGE STATION 1051, STRINGER 11L AND STRINGER 15L. REPAIRED IAW HORIZON AIR EA R-53-422 AND CRJ700 SRM 51-25-01-001-001-A01.
Part: STRUCTURE — CORRODED (E/E BAY DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR AVIONICS BAY DOOR SURROUND INNER SEAL FACE HAS AREAS OF CORROSION AND BARE METAL. REPAIRED IAW REO 670-53-21-158 AND HORIZON AIR EA R-53-427.
Part: SKIN — DAMAGED (TE FLAP) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-21-26-00-001-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-A01.
Part: SKIN — CHAFED (RT NACELLE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND NACELLE AFT CORE COWL HAS TWO STRIPS OF CHAFING DAMAGE ON INBOARD SIDE. REPAIRED IAW REO 71-11-525 AND HORIZON AIR EA R-71-133.
Part: SKIN — NICKED (BS 566) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR FUSELAGE STATION 566, STRINGER 26L HAS NICKED SKIN. REPAIRED IAW REO 670-53-31-063, HORIZON AIR EA R-53-423 AND CRJ700/900 SRM 51-25-01-001-001-A01.
Part: FASTENER — BROKEN (RT WING TE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT WING TRAILING EDGE HAS BROKEN FASTENER AT STATWION WS199.40. REPAIRED IAW CRJ700/900 SRM 51--42-06-001-001-A01.
Part: SKIN — GOUGED (BS 533-581) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR LEFT FUSELAGE STATION 533-581 AT LOWER EDGE OF FORWARD BAGGAGE DOOR, SKIN GOUGED IN THREE PLACES. REPAIRED IAW HORIZON AIR EA R-53-423, REO 670-53-31-063 AND CRJ700/900 SRM 51-25-01-001-001-A01.
Part: DOOR FRAME — GOUGED (BS 310) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE PASSENGER DOOR SURROUND STRUCTURE ON FRAME 310, LOWER ROLLER FITTING NICKED AND GOUGED. REPAIRED IAW REO 670-53-21-160 AND HORIZON AIR EA R-53-421.
Part: TRACK — DAMAGED (BS 1000) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE AFT BAGGAGE DOOR FORWARD DOOR ROLLER TRACK SUPPORT FRAME HAS AREA OF SCRATCHES ON AFT FACE, FUSELAGE STATION 1000. REPAIRED IAW REO 670-53-61-236 AND HORIZON AIR EA R-53-426.
Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND MAIN LANDING GEAR DOOR, AFT TOP HINGE AREA, WEB CRACKED. REPAIRED IAW CRJ700 AMM TASK 32-12-01-000-802-A01.
Part: SKIN — NICKED (BS 1000-1051) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR, RIGHT SKIN BETWEEN STATION 1000.00 AND STATION 1051.30 FROM STRINGER 23R TO 27R HAS MULTIPLE NEW NICKS. REPAIRED IAW REO 670-53-61-232 AND CRJ700 SRM TASK 51-25-01-001-001-A01.
Part: SKIN — CHAFED (BS 980) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR, LOWER SKIN HAS TWO CHAFE MARKS FROM LEAKING SCREWS AT FUSELAGE STATION 980, BLO AND LBL1.5. REPAIRED IAW REO 670-53-00-014, HORIZON AIR EA R-53-428.
Part: FITTING — TOOL DAMAGE (HORIZONTAL STAB) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND HORIZONTAL STABILIZER PIVOT FITTING HAS TOOL MARK. REPARIED IAW HORIZON AIR EA R-55-45 AND REO 670-55-11-031.
Part: SILL — DAMAGED (BS 1000-1047) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE AFT BAGGAGE DOOR SILL, HAS AREAS OF CORROSION ON INNER FACE AND WEAR DAMAGE ON TOP SURFACE, BETWEEN FUSELAGE STATION 1000 TO FUSELAGE STATION 1047. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, HORIZON AIR EA F-53-424, REO 670-53-61-24, REV AND SRM 51-21-16-001-001-A01.
Part: ATTACH FITTING — CORRODED (AILERONS) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND AILERON INBOARD PCU OUTBOARD LUG HAS PITTING CORROSION IN MULTIPLE AREAS. REPAIRED IAW HORIZON AIR EA R-57-138 AND REO 670-57-61-030.
Part: ANGLE — MISSING (BS 581) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR RIGHT HAND FUSELAGE STATION 581, STRINGER 15, ANGLE MISSING AT SIDE SEAT RAIL INTERCOSTAL. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND HORIZON AIR EA R-53-430.
Part: DOOR — DAMAGED (LT MLG) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND WING MAIN LANDING GEAR DOOR REBATE, AFT REBATE IS BENT/DAMAGED. REPAIRED IAW CRH700/900 SRM 51-42-06-001-001-A01.
Part: SKIN — DAMAGED (BS 1000-1047) · airframe 15,175 hrs · 8,672 cycles
YYC - C3 FUSELAGE AFT BAGGAGE DOOR HAS AREAS OF SCRATCHES FORWARD AND AFT FUSELAGE STATION 1000 AND FUSELAGE STATION 1047. REPAIRED IAW REO 670-53-61-196 AND CRJ700 SRM 51-21-16-001-001-A01.
Part: SKIN — CHAFED (LT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND WING, MID SECTION LEADING EDGE PANEL 522BL FROM SS144.94 TO SS249.04 NUMEROUS CHAFE MARKS ON SKIN. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-41-01-101-001-A01.
Part: SKIN — CHAFED (RT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND LEADING EDGE PANEL 631AR HAS CHAFE MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-41-01-101-001-A01 AND SRM 51-25-16-001-001-A01.
Part: ATTACH BRACKET — WORN (FLAP FAIRING) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND FLAP STUB FAIRING 172DR FORWARD ATTACH BRACKET WORN. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01.
Part: SKIN — CHAFED (LT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC C3 LEFT HAND WING, LEADING EDGE 531AL PANEL FROM SS249.04 TO SS337.66 NUMEROUS CHAFE MARKS. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: STRUCTURE — WORN (RT AILERON) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT AILERON OUTBOARD TOP LEADING EDGE WORN BY SEAL, UNDER PANEL 698CT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: DOOR — DAMAGED (RT MLG) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND WING MAIN LANDING GEAR DOOR REBATE, AFT REBATE IS BENT/DAMAGED. REPAIRED IAW CRH700/900 SRM 51-42-06-001-A01.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, FUSELAGE STATION CROSSBEAM UPPER FLANGE IS CORRODED FROM LBL5.50 TO RBL5.50. REPAIRED IAW REO 670-55-045, REV E.
Part: SKIN — CHAFED (RT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND LEADING EDGE PANEL 622BR HAS CHAFED MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-41-01-101-001-A01 AND SRM 51-25-16-001-001-A01.
Part: SKIN — CHAFED (RT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND LEADING EDGE PANEL 622AR HAS CHAFED MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-1-01-101-001-A01 AND SRM 51-25-16-001-001-A01.
Part: SKIN — CHAFED (LT WING LE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND WING, INBOARD LEADING EDGE SKIN PANEL FROM SS 57.00 TO SS 144.00 (522AL) NUMEROUS CHAFE MARKS ON SKIN. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 863-916) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 863 TO FUSELAGE STATION 916. REPAIRED IAW REO 670-53-013, REV A.
Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT HAND SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 785 TO FUSELAGE STATION 830. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 840-863) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 840 TO FUSELAGE STATION 863. REPAIRED IAW REO 670-53-00-013, REV A.
Part: NUT — DAMAGED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR, FUSELAGE STATION 990 BETWEEN STRINGER 25L AND 24R THERE ARE 10 ACH ANCHOR NUTS WITH WORN OUT LOCKING DEVICE. REPLACED IAW CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-23-03-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 916-953) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 916 TO FUSELAGE STATION 953. REPAIRED IAW REO 670-53-00-013 REV A.
Part: SEAT TRACK — CORRODED (BS 850) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT HAND INBOARD SEAT RAIL HAS AREAS OF CORROSION AND GOUGES FROM FUSELAGE STATION 850 TO FUSELAGE STATION 985. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 394) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION AND GOUGES FROM FUSELAGE STATION 394 TO FUSELAGE STATION 440. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — GOUGED (BS 453-480) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF GOUGES FROM FUSELAGE STATION 453 TO FUSELAGE STATION 480. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 715-761) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT HAND SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 715 TO FUSELAGE STATION 761. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT FLOOR SEAT RAIL, FUSELAGE STATION 581.0 - 683.45 HAS FIVE AREAS OF CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 400-570) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 400 TO FUSELAGE STATION 570. REPAIRED IAW REO 670-53-00-013, REV A.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 PASSENGER DOOR AFT SIDE PANEL CRACKED AT FOLDING HANDRAIL BRACKET. REPAIRED IAW REO 670-52-11-104.
Part: SEAT TRACK — CORRODED (BS 570-629) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM STATION 570.40 TO STATION 629. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 683-701) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT FLOOR SEAT RAIL, FUSELAGE STATION 683.45 - 701.45, HAS ONE AREA OF GOUGES AND CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR LEFT HAND FLOOR SEAT RAIL HAS SIX AREAS OF CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL HAS FOUR AREAS OF GOUGES AND CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 700) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT INBOARD SEAT RAIL HAS AREAS OF CORROSION AND GOUGES FROM FUSELAGE STATION 700 TO FUSELAGE STATION 836. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 715-675) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, LEFT HAND OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 715 TO FUSELAGE STATION 675. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 661-571) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM STATION 661 TO STATION 571. REPAIRED IAW REO 670-53-00-013.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 PASSENGER DOOR AFT SIDE PANEL CRACKED AT BACK OF 3RD STEP. REPAIRED IAW CRJ700 SRM 52-11-04-001-A01 AND SRM 51-25-16-001-001-A01.
Part: FITTING — DAMAGED (HORIZONTAL STAB) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 HORIZONTAL STAB, LEFT AND RIGHT PIVOT FITTINGS ANTI ROTATION DEVICE, FITTINGS HAVE ADDITIONAL DAMAGE. REPAIRED IAW REO 670-55-11-001, HORIZON AIR EA R-55-64.
Part: SEAT TRACK — CORRODED (BS 460) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT HAND OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION AT STATION 460. REPAIRED IAW REO 670-53-013.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 PASSENGER DOOR AFT SIDE PANEL CRACKED AT BACK OF 1ST BOTTOM STEP. REPAIRED IAW CRJ700 SRM 51-25-16-001-001-A01 AND SRM 51-41-02-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-571) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM STATION 485 TO STATION 571. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 840-863) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM STATION 840 TO STATION 863. REPAIRED IAW REO 670-53-00-013.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 PASSENGER DOOR FORWARD SIDE PANEL CRACKED AT FOLDING HANDRAIL BRACKET. REPAIRED IAW REO 670-52-11-104.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 PASSENGER DOOR AFT SIDE PANEL CRACKED AT BACK OF TOP STEP. REPAIRED IAW CRJ700 SRM 52-11-04-001-001-A07 AND SRM 51-25-16-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT SIDE SEAT RAIL HAS AREAS OF PITTING CORROSION FROM FUSELAGE STATION 785 TO FUSELAGE STATION 830. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 715-761) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT HAND OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 715 TO FUSELAGE STATION 761. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 394-437) · airframe 11,575 hrs · 8,672 cycles
YYC C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM STATION 394 TO STATION 437. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 675-715) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FUSELAGE STATION 675 TO FUSELAGE STATION 715. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — GOUGED (BS 863-909) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT OUTBOARD SIDE SEAT RAIL HAS AREA OF GOUGES FROM FUSELAGE STATION 863 TO FUSELAGE STATION 909. REPAIRED IAW REO 670-53-00-018.
Part: LANDING GEAR — UNKNOWN (RIGHT) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT HAND MAIN LANDING GEAR SIDE STAY INBOARD END HAS .015 END PLAY. REPAIRED IAW HORIZON AIR EA R-32-220A, SECTION 2 AND REO 670-32-11-189.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT FLOOR SEAT RAIL HAS ONE AREA OF CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTRIOR RIGHT FLOOR SEAT RAIL FUSELAGE STATION 485.0-581.0 HAS THREE AREAS OF CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SKIN — NICKED (BS 1031) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR HAS NICK ON SKIN AT STRINGER 11R, FUSELAGE STATION 1031. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: FASTENER — BROKEN (RT WING) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT WING UPPER SKIN TRAILING EDGE (OUTBOARD OF MULTI FUNCTION SPOILER) HAS BROKE FASTENER. REPAIRED IAW CRJ700/900 SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT FLOOR SEAT RAIL HAS FOUR AREAS OF CORROSION. REPAIRED IAW REO 670-53-00-013, REV A.
Part: STRUCTURE — WORN (RT AILERON) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT AILERON LOWER INBOARD LEADING EDGE WORN BY SEAL, 22" IN FROM INBOARD END. REPAIRED IAW CRJ700/900 51-12-00-001-001-A01 AND SRM 51-25-01-001-A01.
Part: LANDING GEAR — UNKNOWN (LEFT) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT MAIN LANDING GEAR SIDE STAY INBOARD END HAS .018 END PLAY. REPAIRED IAW HORIZON AIR EA R-32-220A AND REO 670-32-11-189.
Part: SEAT TRACK — GOUGED (BS 850-923) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR RIGHT INBOARD SEAT RAIL HAS AREAS OF GOUGES FROM FUSELAGE STATION 850 TO FUSELAGE STATION 923. REPAIRED IAW REO 670-53-00-013, REV A.
Part: FASTENER — LOOSE (RT WING SKIN) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 RIGHT WING UPPER SKIN TRAILING EDGE (INBOARD OF MULTI FUNCTION SPOILER) HAS LOOSE FASTENER. REPAIRED IAW CRJ700/900 SRM 51-42-06-001-001-A01.
Part: SKIN — NICKED (BS 685 S15L) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR HAS NICK ON SKIN AT STATION 685 AND STRINGER 15L. REPAIRED IAW CRH700 SRM 53-00-01-991-803 AND 51-25-01-001-001-A01.
Part: SEAT TRACK — GOUGED (BS 350-485) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR RIGHT FLOOR SEAT RAIL FS350-485.0, RIGHT SH670-32159-1 HAS 2 AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013, REV A.
Part: SEAT TRACK — CORRODED (BS 700) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR, RIGHT INBOARD SEAT RAIL HAS AREAS OF CORROSION AND GOUGES FROM FUSELAGE STATION 700 TO FUSELAGE STATION 836. REPAIRED IAW REO 670-53-00-013, REV A.
Part: STRUCTURE — WORN (LT AILERON) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 LEFT HAND AILERON TOP INBOARD LEADING EDGE WORN BY SEAL UNDER PANEL 598AT, 598BT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
Part: FASTENER — MISSING (BS 295) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE STRUCTURE, STATION 295 AT 12 O'CLOCK POSITION, CLIP IS MISSING 2 RIVETS. REPAIRED IAW CRJ700 SRM 51-42-06-00-001-A01.
Part: FRAME — MISINSTALLED (BS 517) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR RIGHT HAND FRAME AT FUSELAGE STATION 517, BELOW STRINGER 9 HAS RIVET POORLY INSTALLED-SKIN TO FRAME. REPLACED RIVET IAW CRJ700 SRM 51-42-06-001-001-A01.
Part: FRAME — MISINSTALLED (BS 797) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE INTERIOR FRAME AT FUSELAGE STATION 797, STRINGER 14R HAS POORLY INSTALLED RIVET FOR INTERCOSTAL. REPLACED RIVET IAW CRJ700/900 SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — NICKED (COCKPIT) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 COCKPIT INTERIOR PILOTS INBOARD SEAT TRACK HAS SEVERAL NICKS AND SCRATCHES ON INBOARD FLANGE FACE IN THE AFT 6" AREA. REPAIRED IAW CRJ700/900 SRM TASK 53-11-49-101-01-A01 AND SRM TASK 51-25-00-001-001-TA01.
Part: SKIN — CHAFED (BS 974) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 FUSELAGE EXTERIOR, LOWER SKIN HAS CHAFE DAMAGE FROM THE FAIRING STIFFENER AT FUSELAGE STATION 974 AND BLO. REPAIRED IAW REO 67053-00-014 REV (STEP 1, 2 AND 4).
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 COCKPIT INTERIOR PILOTS OUTBOARD SEAT TRACK HAS SEVERAL NICKS ON THE OUTBOARD FLANGE EDGE IN THE AFT 6" AREA. REPAIRED IAW CRJ700/900 SRM TASK 53-11-49-101-001-A01 AND SRM 51-25-00-001-001-A01.
Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 11,575 hrs · 8,672 cycles
YYC - C3 COCKPIT INTERIOR PILOTS INBOARD SEAT TRACK HAS SEVERAL NICKS ON INBOARD FLANGE FACE IN THE FORWARD 6" AREA. REPAIRED IAW CRJ700/900 SRM TASK 53-11-49-101-001-A01 AND SRM 51-25-00-001-001-A01.
2005
Part: STARTER — FAILED (NR 1) · airframe 11,460 hrs · 8,601 cycles
PDX - PUSHBACK FOR FLIGHT 2473, LEFT ENGINE WILL NOT START. ENGINE START STATUS MESSAGE APPEARS BUT THERE IS NO N2 ROTATION. RETURNED TO THE GATE. REPLACED NR 1 STARTER IAW IAM 80-11-01 PGS 401-406, LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: HEAT EXCHANGER — LEAKING (NR 2 HYD SYSTEM) · airframe 11,305 hrs · 8,500 cycles
PDX - ON FLIGHT 2451, 100 MILES OUT OF PDX NR 2 HYDRAULIC SYSTEM FAILED. FLIGHT RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. SHUTOFF VALVE TO NR 2 SYSTEM WAS CLOSED FOR 25-30 MINUTES. MAINTENANCE FOUND SKYDROL LEAKING AT THE EXIT FOR THE HEAT EXCHANGER. REPLACED THE HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. PERFORMED REQUIRED INSPECTIONS FOR ENGINE DRIVEN PUMPS OPERATING WITHOUT FLUID. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: TARGET — OUT OF ADJUST (MLG) · airframe 11,218 hrs · 8,445 cycles
PDX - ON FLIGHT 2451 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. PROX SYSTEM 1 FAULT WAS SHOWN. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE GEAR PROX SENSOR TARGET PX08. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 11,176 hrs · 8,417 cycles
PDX - ON FLIGHT 2451, RETURNED TO THE GATE WITH NR 2 ENGINE HUNG START. MAINTENANCE REPLACED THE NR 2 STARTER AND VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CHIMNEY — DAMAGED (SMOKE DETECTOR) · airframe 10,955 hrs · 8,276 cycles
PDX - FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REPLACED THE CARGO BAY CHIMNEY. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (NR 2 FIRE EXTING) · airframe 10,306 hrs · 7,822 cycles
SEA - NR 2 ENGINE FIRE EXTINGUISHER FAIL CAUTION MESSAGE RECEIVED. MAINTENANCE CLEANED THE CONNECTOR ON THE FIRE EXTINGUISHER BOX. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: SERVO — MALFUNCTIONED (STICK PUSHER) · airframe 10,069 hrs · 7,660 cycles
PDX- FLIGHT NR 2509 - DURING FLIGHT CONTROL CHECK OF ELEVATORS, ELEVATOR MOVEMENT TO UP O=POSITION (NOSE DOWN) REQUIRES MORE THAN NORMAL PRESSURE WITH PRESSURE FELT AGAINST CONTROL COLUMN AND A NOTICEABLE CLICKING. RATCHETING SOUND ASSOCIATED WITH CONTROL COLUMN MOVEMENT. MAINTENANCE REPLACED THE STICK PUSHER SERVO. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2004
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 8,314 hrs · 6,425 cycles
DEN - ON FLIGHT NUMBER 4321, UPON APU STARTUP RECEIVED APU OVERTEMP WARNING. COMPLETED CHECKLIST. MAINTENANCE PERFORMED APU STARTUP ON RAMP, APU STARTED NORMALLY. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ATTACH ANGLE — CRACKED (ZONE 800) · airframe 7,715 hrs · 5,977 cycles
MAIN CABIN DOOR ASSEMBLY TO MAIN CABIN DOOR SHELL AFT ATTACH ANGLE CRACKED APPROXIMATELY IN MIDDLE OF DOOR. REPAIRED IAW HORIZON AIR EA R-52-190 AND REO 670-52-11-072.
Part: BEAM — CORRODED (ZONE 100) · airframe 7,715 hrs · 5,977 cycles
PDX - BEAM FS 280 TOP FLANGE HAS NUMEROUS SPOTS OF CORROSION ON EITHER SIDE OF COCKPIT ENTRANCE. REPAIRED IAW SRM 51-12-00.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 7,715 hrs · 5,977 cycles
PDX - FLOORBEAM FS 280 IS CRACKED TOP FLANGE 12 INCHES FROM CENTER RIGHT SIDE. REPAIRED IAW REO 670-53-11-045 AND HORIZON AIR EA R-55-211.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 7,715 hrs · 5,977 cycles
PDX - BEAM FS 280 HAS A POSSIBLE CRACK LEFT SIDE BELOW T-BRACKET ATTACH POINT FOR SEAT RAIL BEAM. REPAIRED IAW REO 670-53-11-045.
Part: PIN — WORN (ZONE 300) · airframe 7,715 hrs · 5,977 cycles
PDX - HORIZONTAL STAB HINGE BOLT PIVOT PINS HAVE STEPWEAR DAMAGE TO THE ANTI ROTATION LUGS. REPAIRED IAW HORIZON AIR EA R-53-23.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 7,715 hrs · 5,977 cycles
COCKPIT FLOORBEAM WITH CAMLOCK RECEPTACLES ON IT AT JUST FORWARD OF FS 280 HAS CORROSION ON TOP OF C CHANNEL. REPAIRED IAW REO 670-53-1-095 AND SRM 51-42-06-001-001.
Part: STRUCTURE — CORRODED (ZONE 100) · airframe 7,715 hrs · 5,977 cycles
PDX - THE COCKPIT BACK WALL AFT SIDE RIGHT HAS NUMEROUS SPOTS OF CORROSION AT FLOOR LEVEL AT BEAM FS 280. REPAIRED IAW HORIZON AIR EA R-53-211 AND REO 670-53-11-051.
Part: WINDOW — FAILED (ZONE 200) · airframe 7,086 hrs · 5,497 cycles
LAX-ON FLIGHT NR 2547, AT FLIGHT LEVEL 390 WITH WINDOW HEAT ON THE LT SIDE COCKPIT WINDOW SHATTERED. THE CRACK RADIATED FROM FORWARD LOWER CORNER AND INVOLED THE OUTER LAYER. AFTER THE LT WINDOW SHATTERED THERE WAS A HEAT CAUTION MESSAGE. REMOVED AND REPLACED LT SIDE COCKIT WINDOW. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUT — DISENGAGED (ZONE 800) · airframe 6,958 hrs · 5,404 cycles
PDX - FLIGHT 2473 - SERVICE DOOR WILL NOT OPEN PROPERLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-ENGAGED THE INNER AND OUTER UPLOCK STRUT SECTIONS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ROLLER — LACK OF LUBE (SERVICE DOOR) · airframe 6,523 hrs · 5,067 cycles
SEA FLIGHT 2464, GALLEY SERVICE DOOR HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR ROLLERS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
2003
Part: CHIMNEY — DAMAGED (ZONE 200) · airframe 13,979 hrs · 19,989 cycles
PDX- FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY.
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 5,321 hrs · 4,163 cycles
BOI- ON FLIGHT 2430 AFTER LEFT COWL ANTI-ICE ON EN ROUTE, LEFT ENGINE BLEED CAUTION AND LEFT COWL ANTI-ICE CAUTION ON. RAN CHECKLIST. TESTED COWL ANTI-ICE SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 5,135 hrs · 4,030 cycles
ON FLIGHT 2490 FIRE SYSTEM FAULT STATUS MESSAGE. COMPLIED WITH FIM TASK 26-10-00-810-805-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WINDOW — CRACKED (COCKPIT) · airframe 5,097 hrs · 4,001 cycles
SEA- ON FLIGHT 2452 FIRST OFFICER'S SIDE WINDSHIELD SHATTERED JUST AS DESCENT WAS STARTED AT 41,000 FEET. REMOVED AND REPLACED FIRST OFFICER'S RIGHT HAND SIDE WINDOW. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SELECTOR VALVE — FAILED (MLG) · airframe 5,095 hrs · 4,000 cycles
BOI- ON FLIGHT 2547 AIRCRAFT RETURNED TO FIELD DUE TO GEAR DISAGREE WARNING LIGHT AFTER TAKEOFF. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ACTUATOR — LEAKING (LT ENGINE) · airframe 5,059 hrs · 3,971 cycles
PDX- ON FLIGHT 2439 LEFT ENGINE FUEL LEAK. REMOVED AND REPLACED SLAVE COMPRESSOR VARIABLE GEOMETRY ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUT — OUT OF ADJUST (ZONE 800) · airframe 4,609 hrs · 3,640 cycles
ON FLIGHT 2528 MAIN CABIN DOOR WILL NOT OPEN. ADJUSTED COUNTER BALANCE FORWARD GAS STRUT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: COUNTERBALANCE — OUT OF ADJUST (ZONE 800) · airframe 4,609 hrs · 3,640 cycles
ON FLIGHT 2482 MAIN CABIN DOOR WILL NOT OPEN. ADJUSTED MAIN CABIN DOOR AFT COUNTERBALANCE. NO PARTS REPLACE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 4,517 hrs · 3,572 cycles
BOI- ON FLIGHT 2456 UNABLE TO OPEN MAIN CABIN DOOR FROM EXTERNAL HANDLE. CLEANED AND LUBED HINGE AND PINS. NO PARTS REPLACED. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,303 hrs · 3,415 cycles
SMF- ON FLIGHT 2492 SMF TO SEA, DIVERTED TO PDX DUE TO ON GROUND (LEFT BLEED DUCT) WARNING MESSAGE CAME ON. BOTH PACKS SHUTDOWN. AFTER 10 SECONDS THE WARNING WENT OUT, FOLLOWED BY (LEFT BLEED DUCT) CAUTION MESSAGE. THE MANUAL BLEED PROCEDURES PRODUCED NO RESULTS. AIRCRAFT LANDED WITHOUT INCIDENT. RAN BLEED LEAK DETECTION TEST ON BOTH CHANNELS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LOOP — OUT OF POSITION (A/C BAY) · airframe 4,268 hrs · 3,386 cycles
SEA- ON FLIGHT 2512 LEFT BLEED DUCT WARNING MESSAGE FOLLOWED BY LEFT BLEED DUCT CAUTION MESSAGE. SYSTEM AUTO SHUTDOWN. PER CHECKLIST RESTARTED IN MANUAL. FOUND BLEED LOOP TOUCHING LOOSE SHROUD IN AFT EQUIPMENT BAY. RESECURED SHROUD AND ADJUSTED BLEED LOOP TO PROPER CLEARANCE. NO PARTS REPLACED. OPERATIONAL CHEKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SEAL — WORN (ACM) · airframe 4,092 hrs · 3,264 cycles
BOI- ON FLIGHT 2524 AFTER TAKEOFF RECIEVED RIGHT BLEED DUCT WARNING. AUTO SYSTEM TEMPORARY SHUT OFF RIGHT BLEED SYSTEM AND MESSAGE CHANGED TO A CAUTION. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ACM SEALS AND COUPLING. OPEATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 4,061 hrs · 3,235 cycles
BOI- ON FLIGHT 2524 "SMOKE AFT LAVATORY" EICAS WARNING OCCURRED WITH SMOKE DETECTOR ALARM ACTIVATION IN LAVATORY. WARNING DISAPPEARED FOLLOWING PULLING CIRCUIT BREAKERS AS PER CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NO.2 HOT AIR SHUTOFF VALVE. OPERATIONAL CHECKS GOOD.APU IS STILL ON MEL. AIRCRAFT RETURNED TO SERVICE.
Part: APU — LEAKING (APU BAY) · airframe 4,057 hrs · 3,229 cycles
AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED AN AFT LAVATORY SMOKE DETECTOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND OIL IN MIXING MANIFOLD AND VERIFIED THAT THE APU WAS LEAKING OIL. DUCTING WAS CLEANED AND MEL WAS CONTINUED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: APU — LEAKING (APU BAY) · airframe 4,056 hrs · 3,228 cycles
BIL - FLIGHT 2481 - CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE AFT LAVATORY SMOKE DETECTOR SOUNDED. THE CREW COULD SMELL OIL BUT THE ODOR SOON DISSIPATED AND THE WARNING WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND OIL IN THE MIXING MANIFOLD. MAINTENANCE VERIFIED THAT THE APU WAS LEAKING OIL AND THE APU WAS MEL'D. THE DUCTING WAS CLEANED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FAN — FAULTY (CABIN) · airframe 3,993 hrs · 3,179 cycles
SJC-SUP-ON FLIGHT NUMBER 2553, SMELL OF SMOKE FOLLOWED BY A RECIRC FAN FAULT. REMOVED AND REPLACED NR 1 RECIRC FAN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (ZONE 100) · airframe 3,806 hrs · 3,036 cycles
SEA-ON FLIGHT NUMBER 2504, ON ROLLOUT AS NOSE GEAR TOUCHES DOWN, GOT A CAUTION STEERING INOPERATIVE MESSAGE. FOLLOWED APPROPRIATE PROCEDURE. C/W CRJ700-SL-32-019, NOSE WHEEL STEERING CAUTION EXTINGUSHED. NOSE WHEEL STEERING OPERATIONAL CHECK WAS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: VANE — CHAFED (ZONE 500) · airframe 3,716 hrs · 2,970 cycles
CKB - LEFT INBOARD FLAP VANE HAS THREE MINOR CHAFES ON LEADING EDGE. REPAIRED IAW WVAC EO 601R-57-3975.
Part: BLADE — MISSING (ZONE 300) · airframe 3,716 hrs · 2,970 cycles
CKB - RIGHT HAND AFT FUSELAGE VENT IS MISSNG ONE RAM AIR EXHAUST DUCT BLADE. REPAIRED IAW WVAC EO 601R-21-3960.
Part: RIVET — MISSING (ZONE 600) · airframe 3,716 hrs · 2,970 cycles
CKB - UPPER AFT RIGHT WING HAS A RIVET MISSING AT WS 170.83. REPAIRED IAW DRJ 700 SRM 51-42-06.
Part: PANEL — CRACKED (ZONE 300) · airframe 3,588 hrs · 2,885 cycles
PDX-NUMEROUS NICKS AND SCRATCHES AROUND EXTERNAL AIR PANEL. REPAIRED IAW CRJ700 NDT MANUAL 51-20-06.
Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 3,158 hrs · 2,597 cycles
PDX ON FLIGHT 2446- AFTER TAKE OFF LEFT ENGINE BLEED CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PACK INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULKHEAD — DAMAGED (ZONE 200) · airframe 3,158 hrs · 2,597 cycles
PDX- AFT PRESSURE BULKHEAD FEED THROUGH ORIFICE FOR NR 2 HYDRAULIC EDP PRESSURE LINE IS ELONGATED. REPAIRED IAW REO 670-53-61-034 AND 670-53-51-034.
Part: WARNING SYSTEM — MALFUNCTIONED (FIRE DETECTION) · airframe 2,991 hrs · 2,477 cycles
TUS-ON FLIGHT NUMBER 2535, INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE, USUALLY ASSOCIATED WITH LIGHT TURBULENCE AT FL370 AND FL390. INTERROGATED MDC, NO FAULT FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
2002
Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 2,981 hrs · 2,480 cycles
PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE HPT 1 BLADE MISSING 20 PERCENT SPAN. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION OF THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS.
Part: CARTRIDGE — FAILED (FUEL SYSTEM) · airframe 2,820 hrs · 2,348 cycles
BOI- TRANSFER PUMP CAUTION AND RIGHT TRANSFER PUSH LIGHT INDICATOR FAIL. SAME RESULTS WITH LEFT TRANSFER PUSH LIGHT SELECTED AND AUTO OVERRIDE SELECTED. PROBLEM CLEARED IN 30 MINUTES. REMOVED AND REPLACED BI-CROSSFLOW PUMP CARTRIDGE.
Part: ACM — FAILED (A/C BAY) · airframe 2,795 hrs · 2,329 cycles
PDX- FOLLOWING ENGINE START CABIN AND COCKPIT FILLED WITH SMOKE FROM AIR DUCTS. RECEIVED SMOKE AFT LAVATORY WARNING. RIGHT PACK AUTO FAIL MESSAGE FOLLOWED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CARTRIDGE — FAILED (FUEL SYSTEM) · airframe 2,773 hrs · 2,313 cycles
BOI- TRANSFER PUMP CAUTION MESSAGE WITH ASSOCIATED LEFT FUEL CROSS/LOW SWITCH LIGHT INDICATING "FAIL" ANYTIME FUEL TANK IMBALANCE EXCEEDS 200 POUNDS. REMOVED AND REPLACED BI-CROSSFLOW PUMP CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 2,659 hrs · 2,226 cycles
PDX - CREW RECEIVED A LEFT FUEL LOW PRESSURE CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 1,582 hrs · 1,385 cycles
BOI - CREW REPORTS FUEL LEAK UNDER THE BELLY OF THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,476 hrs · 1,304 cycles
PDX- MESH CAGE AT DOOR OPENING DAMAGED. REMOVED AND REPLACED SMOKE DETECTOR CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PROXIMITY SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 898 hrs · 862 cycles
BOI - AIRCRAFT RETURNED TO FIELD WHEN SERVICE DOOR CAUTION ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED THE SERVICE DOOR PROXIMITY SENSOR IAW AMM 52-70-06. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: COUPLING — FAILED (CENTER TANK) · airframe 825 hrs · 803 cycles
EUG - CREW RECEIVED FUEL EJECTOR CAUTION LIGHT AND FUEL IMBALANCE, RIGHT TANK LOW CAUTION MESSAGE AND CENTER TANK BEGAN TO TAKE ON FUEL. THE CENTER TANK HAD OVER 4500 LBS OF FUEL UPON LANDING. MAINTENANCE REPLACED THE FAILED RIGHT WIGGINS CLAMP AND RIGHT PRIMARY EJECTOR FUEL FEED TUBE IAW CRJ 700 MAINTENANCE MANUAL. LEAK CHECK IS GOOD. ALL RII ITEMS WERE COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 776 hrs · 757 cycles
FRESNO - ON FLIGHT FROM EUGENE TO LA, FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED TO FRESNO AND CREW COMPLIED WITH EMERGENCY ABNORMAL CHECKLIST. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT DOWN FOR MAINTENANCE. REPLACED RIGHT WINDSHIELD IAW CRJ-700 MM 56-11-01-000-801-A01. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 713 hrs · 708 cycles
SMF - SMOKE AFT LAV MASTER WARNING MESSAGE CAME ON JUST AFTER TAKEOFF. INSPECTED LAVATORY AND FOUND NO EVIDENCE OF FIRE OR SMOKE. RESET SMOKE DETECTOR. GROUND RAN AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
2001
Part: STRIKER — DAMAGED (PAX DOOR) · airframe 635 hrs · 640 cycles
PDX - MAIN CABIN DOOR SEAL STRIKER IS DAMAGED ALONG THE AFT EDGE OF OPENING. REPAIRED MAIN CABIN DOOR APERTURE SEAL STRIKER IAW EA R-53-11.
Part: PSEU — FAULTY (E/E BAY) · airframe 545 hrs · 562 cycles
PDX - AFTER TAKEOFF AND GEAR AND FLAP/SLAT RETRACTION (PROX SYSTEM MESSAGE). ON APPROACH IN PDX SLAT/FLAP EXTENSION NO CHANGE AFTER GEAR HANDLE SELECTED DOWN (PROX SYSTEM MESSAGE) WENT OUT. LANDED WITHOUT INCIDENT. REPLACED PSEU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PANEL — DEFECTIVE (FUSELAGE) · airframe 510 hrs · 528 cycles
GEG- FUELER REPORTED ELECTRICAL SMELL COMING FROM REFUEL/DEFUEL PANEL. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRIKER — DAMAGED (PAX DOOR) · airframe 468 hrs · 492 cycles
PDX-MAIN CABIN DOOR STRIKER DAMAGED MIDWAY ALONG FORWARD LENGTH OF DOOR APERTURE. REPAIRED IAW HORIZON AIR EA R-53-06.
Part: SEAL — DENTED (PAX DOOR) · airframe 231 hrs · 247 cycles
PDX - MAIN CABIN DOOR SEAL MATING SURFACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-03.
Part: SEAL — DENTED (PAX DOOR) · airframe 231 hrs · 247 cycles
PDX - MAIN CABIN DOOR SEAL MATING SURFACE DENTED MIDWAY ALONG THE AFT LENGH OF DOOR APERTURE. REPAIRED IAW EA R-53-03