N879AS
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
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.
292 reports on file, 2002-12-15 – 2019-12-18.
Part: REVEAL — BROKEN (CABIN) · airframe 39,450 hrs · 36,470 cycles
CABIN INNER LINER PANEL 261ALW INNER WINDOW REVEAL SLIDE ATTACHMENT POINT IS BROKEN AND DETACHED (C-CHECK) RO:12/24/2019REPLACED CABIN INNER LINER PANEL 261ALW INNER WINDOW REVEAL IAW ZODIAC AEROSPACE CMM.
Part: SKIN — ERODED (RT AILERON) · airframe 39,450 hrs · 36,470 cycles
RH AILERON UPPER SKINN SURFACE ABOVE N0. 2 AND NO. 3 HINGE BOLTS IS PEELED BACK AWAY FROM THE AILERON BETWEEM WS 317.85 AND WS 321.32 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED DAMAGED AILERON SKIN IAW CRJ 200 SRM AND TASK CARD. NO WEIGHT CHANGE REQUIRED. M-337 ATTACHED
Part: ATTACH FITTING — CRACKED (BS 621 BULKHEAD) · airframe 39,450 hrs · 36,470 cycles
CRACK CONDITION FOUND IN THE AREA OF THE REPAIR REF 601R-53-61-1230 FS 621 BULKHEAD LINTEL AREA . 1' LONG IN THE RADIUS OF THE CLEAT ATTACHED TO LINTEL FITTING AND A SHEARED FASTNER ALSO COMMON TO FS 625.30 AND LINTEL FITTING (C-CHECK) RO:12/24/2019REPAIRED CRACK CONDITION AND DAMAGE TO THE REPAIR AT FS 621 BULKHEAD AREA IAW BOMBARDIER REO COMPLIED WITH TASK CARD, M-337 ATTACHED.
Part: STRINGER — CORRODED (BS 333-349) · airframe 39,450 hrs · 36,470 cycles
FOUND STR 27 TO BE CORRODED BETWEEN FS 333 AND FS349 REPAIRED STR 27 AT FS 333- 349 IAW SRM.
Part: BUTTSTRAP — CORRODED (BS 333) · airframe 39,450 hrs · 36,470 cycles
BUTTSTRAP AT FS 333 IS CORRODED IN SEVERAL LOCATIONS BETWEEN STRINGER 24L AND 24R COMPLIED WITH MAJOR REPAIR OF BUTTSTRAP AT F.S. 333 IAW REO AND SKYWEST TASK CARD MAJOR REPAIR FORM 337 ATTACHED. 1.2 LBS REMOVED 1.8 LBS ADDED FOR A + .7 LBS ADDED
Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 39,450 hrs · 36,470 cycles
RIGHT WING ANTI-ICE DUCT SUPPORT BRACKET UNDER LEADING EDGE PANEL 630AZ WAS CRACKED. REMOVED AND REPLACED DUCT SUPPORT BRACKET IAW AMM.
Part: BRACKET — CRACKED (LT WING) · airframe 39,450 hrs · 36,470 cycles
LEFT WING ANTI-ICE DUCT SUPPORT BRACKET UNDER LEADING EDGE PANEL 520DZ WAS CRACKED. REMOVED AND REPLACED THE DUCT BRACKET IAW AMM.
Part: FLOORBEAM — CORRODED (BS 424) · airframe 39,450 hrs · 36,470 cycles
FOUND PITTING CORROSION ON EDGE OF LBL/RBL 27 FLOOR BEAM CAPS AT FS 424. (C-CHECK) RO:12/24/2019BLENDED COROSION IAW CRJ-200-REO FOUND TO BE OUT OF LIMITS, DISPOSITION FOR CORROSION BLENDS FOUND ON REO, COMPLIED WITH ALL REQUIRED STEPS.
Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 39,450 hrs · 36,470 cycles
F.S. 621 BULKHEAD LOWER AFT STIFFENER O/B OF LBL 36 IS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM.
Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 39,450 hrs · 36,470 cycles
LEFT ENGINE THRUST REVERSER CASCADE AT THE 12 O'CLOCK POSITION WAS CRACKED. REMOVED AND REPLACED THE LT ENGINE THRUST REVERSER IAW AMM.
Part: ANGLE — CORRODED (BS 621-625) · airframe 39,450 hrs · 36,470 cycles
RH FS621.0 TO FS625 UPPER INTERCOSTAL ANGLE AT BL 45, STRINGER 14R, WL 97.5 IS CRACKED APPROX 0.3" LONG. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED INTERCOSTAL P/N 601-35012-52 WITH SERVICEABLE INTERCOSTAL IAW CRJ200 SRM.
Part: ANGLE — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
RIGHT CAP ANGLE CORRODED BETWEEN FS409.00 AND 409.00+112 AT RBL 9.00 REMOVED AND REPLACED CORRODED CAP ANGLE WITH NEWLY FABRICATED CAP ANGLE AT RBL9 BETWEEN FS409 AND FS409+112 IAW SRM AND DRAWING .
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
RH CABIN FLOOR SILL CORRODED FROM FS409 TO FS409.00+112. REPAIRED CORRODED AREAS AS REQUIRED COMMON TO RH FLOOR SILL FROM FS409.00 TO FS 409+112 IAW REO ALL STEPS COMPLETE.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
LH FLOOR SILL CORRODED BETWEEN FS409.00 AND 409.00+112. REPAIRED CORRODED AREAS AS REQUIRED COMMON TO LH FLOOR SILL FROM FS409.00 TO FS409+112 IAW REO
Part: FRAME — CORRODED (BS 333) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS333.00 CORRODED IN SEVERAL LOCATION BETWEEN STGR24R AND STGR24L AND BETWEEN STGR20L TO STGR21L. COMPLIED WITH MAJOR REPAIR UPON FURTHER INVESTIGATION FOUND FRAME BETWEEN STRINGER 24R AND 24L TO BE CORRODED AT FS 319.70 AND CORRODED AT FS 333 BETWEEN STRINGER 22L AND 23L. REMOVED CORRODED FRAME SECTOR AT FS 319.70 AND INSTALLED NEW SERVICEABLE FRAME SECTOR IAW SRM 51-42-06 AND 51-42-21. BLENDED FRAME AT FS 333 BETWEEN STRINGER 22L AND 23L IAW SRM AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM AND TASK CARD MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (BS 349-409) · airframe 39,450 hrs · 36,470 cycles
RH CABIN FLOOR SILL CORRODED FROM FS349.00 TO FS409.0 ALONG RBL 42. REMOVED CORROSION FROM CABIN FLOOR RBL42 AT FS349 TO FS409 IAW REO.
Part: FLOOR SUPPORT — OUT OF LIMITS (BS 424) · airframe 39,450 hrs · 36,470 cycles
R/H CABIN FLOOR SILL PANEL AT F.S.424.00 IS OUT OF LIMITS OF REO 601R-53--41-666 FOUND REMAINING THICKNESS TO BE WITHIN LIMITS PER REO.
Part: ANGLE — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
LH CAP ANGLE CORRODED BETWEEN FS409.00 AND 409.00+112 AT LBL 9.00 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED CORRODED CAP ANGLE WITH NEWLY FABRICATED CAP ANGLE AT LBL9 BETWENN FS409 AND FS409+112 IAW CRJ200 SRM DRAWING. TASK CARD ISSUED, M-337 COMPLETED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
LH FLOOR SEAT TRACK CORRODED FROM APPRX FS559+8.00 TO FS559+91.00 AT LBL9 (C-CHECK) RO:12/24/2019REPLACED L/H FLOOR SEAT TRACK IAW BOMBARDIER REO.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR INTERCOSTAL BETWEEN STGR 17L TO 16L AT F.S. 310 IS CORRODED. REMOVED&REPLACED PAX DOOR INTERCOSTAL AT STR16 BETWEEN F.S. 295-F.S.310L IAW CRJ 200 SRM COMPLETED AND FORM 337 ATTACHED PART FOR PART REPLACEMENT NO WT CHANGE
Part: SEAT TRACK — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
RH FLOOR SEAT TRACK CORRODED FROM APPRX FS559+8.00 TO FS559+91.00 AT RBL9 (C-CHECK) RO:12/24/2019REPLACED R/H FLOOR SEAT TRACK IAW BOMBARDIER REO.
Part: FRAME — CORRODED (BS 621) · airframe 39,450 hrs · 36,470 cycles
FRAME STRAP AT FS621.00 CORRODED BETWEEN APRROX STGR26R AND STGR26L. REPAIRED CORROSION DAMAGE ON F.S.621 FRAME STRAP BETWEEN STGR25L AND 25R IAW BOMBARDIER REO.
Part: FRAME SPLICE — CORRODED (BS 621) · airframe 39,450 hrs · 36,470 cycles
FRAME AND SPLICE CORRODED AT FS 621.00 BETWEEN STR 26R AND STR 26L. (C-CHECK) RO:12/24/2019REPAIRED CORROSION DAMAGE FRAME SPLICE AT F.S. 621 BY BLENDING IAW CRJ200 SRM AND FOUND TO BE WITHIN LIMITS IAW CRJ200 SRM.
Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR AFT ANCHOR FITTING IS CORRODED AROUND BOLT HOLES. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING IAW AMM.
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,450 hrs · 36,470 cycles
RH FLOOR SEAT TRACK CORRODED FROM APPRX FS409+126 TO FS559+8.00 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED, FABRICATED AND INSTALLED R/H FLOOR SEAT TRACK FROM FS409+126 TO FS559+8.00 AT RBL9 IAW BOMBARDIER REO.
Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 39,450 hrs · 36,470 cycles
LH FLOOR SEAT TRACK CORRODED FROM APPRX FS399 TO FS409+126 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED LH SEAT TRACK FROM FS399 TO FS409+126 AT LBL9 IAW CRJ-200 AMM.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
RH FLOOR SEAT TRACK CORRODED FROM APPRX FS364 TO FS409 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED R/H FLOOR SEAT TRACK FROM FS364 TO FS409 IAW CRJ200 AMM.
Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
FWD PAX DOOR ANCHOR FITTING IS CORRODED AROUND BOLT HOLES. REPLACED FWD PAX DOOR ANCHOR FITTING IAW AMM.
Part: STRAP — CORRODED (BS 424) · airframe 39,450 hrs · 36,470 cycles
PRESSURE FLOOR TENSION STRAPS CORRODED ON UPPER SURFACE AT FS 424.00 LBL 27.0 TO LBL 36.0 AND RBL 27.0 TO RBL 36.0 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED PRESSURE FLOOR TENSION STRAPS AT F.S. 424.00 LBL/RBL 27 TO 36 IAW CRJ 200 SRM.
Part: PLATE — CORRODED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
FWD PAX DOOR SERATED PLATE IS CORRODED. REPLACED FWD PAX DOOR SERATED PLATE IAW AMM.
Part: FRAME — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS 559.00+112 CORRODED BETWEEN STGR25. REMOVED CORROSION AND REPLACED SPLICE ANGLE IAW SRM.
Part: PLATE — CORRODED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
AFT PAX DOOR SERRATED PLATE IS CORRODED ON THE AFT SIDE. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED AFT PAX DOOR SERRATED PLATE IAW AMM.
Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 39,450 hrs · 36,470 cycles
RH FLOOR SEAT TRACK CORRODED FROM APPRX FS399 TO FS409+126 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED RH SEAT TRACK AT FS399 TO FS409+126 RBL IAW CRJ-200 AMM.
Part: BRACKET — CORRODED (BS 319) · airframe 39,450 hrs · 36,470 cycles
RH LOWER FRAME BRACKET CORRODED AT FS 319.70 AND STRG18R. REMOVED AND REPLACED R/H LOWER FRAME BRACKET IAW SRM.
Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
FWD PAX DOOR ANCHOR FITTING IS CRACKED ON THE FWD SIDE. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED FWD PAX DOOR ANCHOR FITTING IS CRACKED ON THE FWD SIDE. IAW AMM.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 39,450 hrs · 36,470 cycles
RIGHT CABIN FLOOR SILL UPPER SURFACE RBL36.0 TO RBL 45.0 FS 409+128 TO FS 559.00 HAS AREAS OF CORROSION. REMOVED CORROSION ON R/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS 559 IAW REO DISPOSITION 1.1 AND 1.2. .055 ORIGINAL THKNESS -.008 = .047 REMAINING.
Part: FRAME — CORRODED (BS 605) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS 605.00 CORRODED BETWEEN STGR16R AND STGR17R. (C-CHECK) RO:12/24/2019BLENDED CORROSION ON F.S.605 FRAME AT STGR 17R - 16R IAW CRJ200 SRM, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW CRJ200 SRM. ORIGINAL FRAME THICKNESS 0.050" MATERIAL REMOVED: 0.001", REMAINING FRAME THICKNESS: 0.049" CALIBRATED TOOL# WVACTENG4886, CAL: 10-JUN-19, CAL DUE: 30-JUN-19
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
LH FLOOR SEAT TRACK CORRODED FROM APPRX FS364 TO FS409 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACEDL/H FLOOR SEAT TRACK FROM FS364 TO FS409 IAW CRJ200 AMM.
Part: STRAP — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
PRESSURE FLOOR TENSION STRAP SMALL AREA OF CORROSION ON UPPER SURFACE FS 559.00 BETWEEN BL 0.0 AND LBL9.0. BLENDED CORROSION ON PRESSURE FLOOR STRAP AT FS599.0 BETWEEN BL0.0 TO LBL9.0 IAW SRM ORIGINAL THICKNESS .063" REMOVED .005" LEAVING .058".
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,450 hrs · 36,470 cycles
LH FLOOR SEAT TRACK CORRODED FROM APPRX FS409+126 TO FS559+8.00 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED LH FLOOR SEAT TRACK FROM FS409+126 TO FS559+8 AT LBL9 IAW BOMBARDIER REO.
Part: BRACKET — CORRODED (BS 349) · airframe 39,450 hrs · 36,470 cycles
RIGHT LOWER FRAME BRACKET CORRODED AT BS 349 AND STRINGER 18R. CORROSION WAS FOUND ON THE DOUBLER AFTER REMOVING THE RT LOWER FRAME BRACKET AT BS 349 AND STRINGER 18R IAW SRM. DOUBLER WAS REPAIRED IAW SRM.FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM AND LOWER FRAME RT BRACKET RE-INSTALLED IAW SRM.
Part: FRAME — CORRODED (BS 605) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS 605.00 CORRODED BETWEEN APPROX STGR 25R AND STGR 24L. REPAIRED FRAME AT FS 605 IAW SRM
Part: FRAME — CORRODED (BS 589) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS 589.00 CORRODED BETWEEN APPROX STGR 26R AND STGR 25L. REMOVED AND REPLACED FRAME SECTOR AT F.S. 589.00 BETWEEN STR 26R AND STR 25L IAW SRM COMPLIED WITHMAJOR REPAIR TASK CARD MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 39,450 hrs · 36,470 cycles
LH CABIN FLOOR SILL UPPER SURFACE LBL 36.0 TO LBL 45.0 FS 409+128 TO FS 559.00 HAS AREAS OF CORROSION. COMPLIED WITH MAJOR REPAIR FLOOR-SILL UPPER SURFACE CORROSION AT LBL 36.0 TO LBL 45.0, BETWEEN FS. 409+128 TO 559.00 IAW REO AND TASK CARD MAJOR REPAIR.
Part: CAP — DENTED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR FWD AND AFT UPPER CORNER CAPS DENTED AND FASTENER CHAFED. COMPLIED WITH REO. REF CONTINUATION CARD FOR WORK PERFORMED.
Part: RETAINER — CORRODED (PAX DOOR SEAL) · airframe 39,450 hrs · 36,470 cycles
UPPER RH CORNER OF PAX DOOR SEAL RETAINER HAS AREA OF CORROSION (C-CHECK) RO:12/24/2019REMOVED AND REPLACED RH CORNER OF PAX DOOR SEAL RETAINER IAW CRJ-200 SRM & SRM REO
Part: PLATE — CHAFED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR FWD CENTERING PLATE CHAFED. REMOVED CHAFE DAMAGE. MAX DEPTH OF DAMAGE MEASURED AT ,015" FOUND TO BE WITHIN LIMITS IAW REO.
Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 39,450 hrs · 36,470 cycles
SERVICE DOOR INNER HANDLE CHAFED. (C-CHECK) RO:12/24/2019REPAIRED AREA IAW CRJ 200 SRM REFERENCE CONTINUE CARD FOR WORK PERFORMED.
Part: FLAP — CHAFED (PAX DOOR) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR PRESSURE VALVE FLAP CHAFED BY ICE BREAK CABLE. (C-CHECK) RO:12/24/2019REPAIRED PAX DOOR PRESSURE VALVE FLAP IAW REO.
Part: BRACKET — CRACKED (WINDOW POST) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDE WINDSHIELD AFT SIDE POST BRACKET WAS CRACKED. REMOVED AND REPLACED THE WINDSHIELD SIDE POST BRACKET.
Part: STIFFENER — CRACKED (RT WING) · airframe 39,450 hrs · 36,470 cycles
R/H WING AUX. SPAR ASSEMBLY CAP IS CRACKED IN TWO LOCATIONS. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED R/H WING AUX. SPAR ASSEMBLY CAP IAW CRJ 200 SRM LOCATE AND DRILL AND SRM HI LITE.
Part: WINDOW POST — CRACKED · airframe 39,450 hrs · 36,470 cycles
LEFT SIDE WINDSHIELD AFT SIDEPOST BRACKET IS CRACKED. REMOVED AND REPLACED THE LT SIDEPOST BRACKET IAW AMM.
Part: FITTING — CRACKED (RT WING) · airframe 39,450 hrs · 36,470 cycles
R/H WING AUX. SPAR ASSEMBLY FITTING IS CRACKED AT AFT SIDE MLG TRUNNION. REMOVED AND REPLACED THE RT AUX SPAR FITTING ASSEMBLY.
Part: FRAME — CORRODED (BS 349) · airframe 39,450 hrs · 36,470 cycles
FRAME AT FS 349.00 CORRODED BETWEEN STGR25R AND STGR25L. REMOVED AND REPLACED FRAME AT FS 349 IAW CRJ200 SRM AND TASK CARD.
Part: SEAT TRACK — FATIGUED (BS 495-535) · airframe 39,450 hrs · 36,470 cycles
LH ISDEWALL SEAT TRACK AT FS 495 TO FS 535 PN 601R38312-131 REQUIRES FABRICATION REF CAMP # 19878532 FOR REPLACEMENT/FABRICATION IF NECESSARY OF SEAT TRACK.
Part: WINDOW POST — CRACKED (RIGHT) · airframe 39,450 hrs · 36,470 cycles
RIGHT WINDSHIELD SIDE POST SUPPORT SHOWS SIGNS OF A CRACK WHERE STRINGER 12R PASSES THRU. NEED NDT TO VERIFY. (C-CHECK) RO:12/24/2019 COMPLIED WITH MAJOR REPAIR BY REMOVING AND REPLACING RH WINDSHIELD SIDE POST SUPPORT IAW CRJ 200 SRM SKYWEST TASK CARD ISSUED AND MAJOR REPAIR FORM 337 COMPLETED. NO WEIGHT CHANGE REQUIRED, PART FOR PART REPLACEMENT
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK HAS AREAS OF CORROSION FROM BS 364 TO BS 409+18. REPAIRED BY REMOVING MINOR CORROSION IAW SRM WITHIN LIMITS IAW SRM REF CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL HAD AREAS OF CORROSION FROM BS 349 TO 364. REMOVED THE CORROSION AND RESTORED THE FINISH IAW SRM.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK WAS CORRODED, BS 364 TO 409+18. REMOVED THE CORROSION IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM.
Part: SEAT TRACK — CORRODED (BS 546-559) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CHANNEL WAS CORRODED IN AREAS FROM BS 546 TO 559+33. REMOVED CORROSION FROM THE SEAT TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CORRODED FROM FS409+18 TO FS409+112. (C-CHECK) RO:12/24/2019FABBED AND REPLACED LEFT SIDEWALL SEAT TRACK FROM FS409+18 TO FS409+112. IAW REO REF CONTINUE CARD FOR DETAILS
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS409+18 TO FS409+70. (C-CHECK) RO:12/24/2019REPAIRED BY REMOVING MINOR CORROSION IAW SRM REF CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CHANNEL CORRODED IN AREAS FROM BS 559+33 TO 559+48. REMOVED AND REPLACED THE SEAT TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK WAS CORRODED FROM BS 444 TO 495. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 546-559) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED FROM BS 546 TO 559+48. FABRICATED AND REPLACED THE SEAT TRACK IAW REO.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK AT BS 349 HAD A CORRODED ANGLE AT THE BEGINNING OF THE TRACK. REPAIRED THE SEAT TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (BS 495-535) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CORRODED FROM FS495 TO FS535. REMOVED FABRICATED AND INSTALLED L/H #5 SIDE SEAT TRACKIAW BOMBARDIER REO.
Part: SEAT TRACK — CORRODED (BS 496-546) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK WAS CORRODED IN AREAS FROM BS 496 TO 546. REPAIRED THE SEAT TRACK IAW REO. REMAINING THKNESS WAS .038 OUT OF .040.
Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK WAS CORRODED FROM BS 409+112 TO 444. BLENDED THE CORROSION IAW SRM.
Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CORRODED FROM FS 409+112 TO FS444. REMOVED AND REPLACED LEFT SIDEWALL SEAT TRACK CORRODED FROM FS 409+112 TO FS444.IAW AMM REF CONTINUE CARD FOR DETAILS
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS409+18 TO FS409+70. REPAIRED BY REMOVING MINOR CORROSION IAW SRM WITHIN LIMITS IAW SRM.
Part: SEAT TRACK — CORRODED (BS 449-496) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK WAS CORRODED IN AREAS FROM BS 449 TO 496. BLENDED THE CORROSION ON THE SEAT TRACK CHANNEL IAW SRM.
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS409+70 TO FS409+111. REPAIRED BY REMOVING MINOR CORROSION IAW SRM REF CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED FROM BS 409+112 TO 444. REMOVED AND REPLACED THE SEAT TRACK IAW AMM, SRM, AND T/R.
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED FROM FS409+18 TO FS409+112. REMOVED AND REPLACED THE RIGHT SIDEWALL SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS409+112 TO FS444. (C-CHECK) RO:12/24/2019REPAIRED BY REMOVING MINOR CORROSION IAW SRM REF CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CORRODED FROM FS444 TO FS495. (C-CHECK) RO:12/24/2019LOCATED DRILLED AND INSTALLED NEW SERVICABLE L/H SIDEWALL SEAT TRACK IAW CRJ 200 SRM AND AMM
Part: SEAT TRACK — CORRODED (BS 500-546) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED FROM BS 500 TO 546. FABRICATED AND REPLACED THE SEAT TRACK IAW REO REV-C, REPAIR B.
Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS444 TO FS495. (C-CHECK) RO:12/24/2019REMOVED CORROSION AT LH SIDE SEAT-TRACK BETWEEN FS.444 AND FS.495 IAW-CRJ 200 SRM
Part: SEAT TRACK — CORRODED (BS 559) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS559+28 TO FS559+80. (C-CHECK) RO:12/24/2019BLENED CORROSION ON LH SIDEWALL SEAT TRACK IAW CRJ-200-SRM.ALL OTHER REF ON CONTINUATION CARD.
Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS409+70 TO FS409+112. REPAIRED BY REMOVING MINOR CORROSION IAW SRM WITHIN LIMITS IAW SRM.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CORRODED FROM BS 364 TO 409+18. LOCATED, MATCHED DRILLED, AND INSTALLED A NEW SERVICABLE SEAT TRACK IAW SRM AND AMM.
Part: SEAT TRACK — CORRODED (BS 535-559) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS535 TO FS559+28. REPAIRED BY REMOVING MINOR CORROSION IAW SRM REF CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 494-535) · airframe 39,450 hrs · 36,470 cycles
LEFT SIDEWALL SEAT TRACK CHANNEL IS CORRODED IN AREAS FROM FS494 TO FS535. BLENDED CORROSION ON LH SIDEWALL SEAT TRACK CHANNEL IN AREAS BETWEEN FS494 TO FS535 IAW CRJ-200-SRM REF ALL OTHER STEPS ON CONTINUATION CARD. BLEND WITHIN LIMITS.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 39,450 hrs · 36,470 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED FROM FS364 TO FS409+18. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.
Part: SKIN — CHAFED (LT AILERON) · airframe 39,450 hrs · 36,470 cycles
L/H AILERON UPPER LEADING EDGE SKIN WS 341 TO WS 353 HAS CHAFING DAMAGE. REPAIRED L/H AILERON UPPER L/E SKIN W.S. 341 TO W.S. 353 IAW REO.
Part: ANGLE — CRACKED (BS 280) · airframe 39,450 hrs · 36,470 cycles
BS 280, STRINGER 3L ANGLE WAS CRACKED, 1 INCH IN LENGTH. REMOVED AND REPLACED BOTH ANGLES IAW SRM.
Part: DUCT — CRACKED (APU AIR INTAKE) · airframe 39,450 hrs · 36,470 cycles
APU AIR INTAKE UPPER DUCT HAD SERVERAL CRACKS. REMOVED AND REPLACED THE UPPER COOLING AIR INTAKE DUCT IAW AMM.
Part: SKIN — CORRODED (LT WING) · airframe 39,450 hrs · 36,470 cycles
LH WING LWR PLANK 540BB HAS CORROSION IN THE CRITICAL AND NON CRITICAL AREAS. REPAIRED AREA IAW REO.
Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 39,450 hrs · 36,470 cycles
FOUND REAR PRESSURE BULKHEAD WEB FWD FACE HAS 7 CHAFED AREAS .200 LONG BY .200 WIDE .003 DEEO. 6 AT WL105 LBL27.50 LBL18 RBL9.50 RBL18 RBL27.50 RBL36.20 AND 1 BETWEEN BL0.0 & LBL9.50 WL85 ALL MARKED ON RPB WEB (C-CHECK) RO:12/24/2019REPAIRED PRESSURE BULKHEAD CHAFE DAMAGE IAW BOMBARDIER REO.
Part: PANEL — CRACKED · airframe 39,450 hrs · 36,470 cycles
PANEL 281HLW HAS CRACK ON CORNER EDGE. REPAIRED.
Part: SKIN — CRACKED (BS 169-173) · airframe 39,450 hrs · 36,470 cycles
SKIN IS CRACKED AT THE TRU DOOR AFT LATCH. CRACK IS APPROX 3/4 INCH LONG. REMOVED AND REPLACED SKIN AT THE TRU DOOR AFT LATCH. BS 169 AND 173.5 IAW SRM. AND DRAWING.
Part: PANEL — CRACKED · airframe 39,450 hrs · 36,470 cycles
PANEL 282 ARW HAD THREE CRACKS ON EDGES OF PANEL.
Part: BULKHEAD WEB — DENTED (BS 621) · airframe 39,450 hrs · 36,470 cycles
FOUND REAR PRESSURE BULKHEAD WEB HAS 2 AREAS HAS MULTIPLE INDICATIONS NOTED 1) BL0.0 WL132-126 50% FSH & 2) LBL9.50 WL74-75.5 70%FSH BOTH FAILED NDT INSPECTION MARKED ON RPB WEB. REPAIRED 2 AREASON REAR PRESSURE BULKHEAD IAW REO.
Part: ATTACH BRACKET — CHAFED (RT WING TE) · airframe 39,450 hrs · 36,470 cycles
R/H WING INBD WING TRAILING EDGE STUB FAIRING ATTACH BRACKET IS CHAFED/WORN BEYOND LIMITS AT WS 48. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED R/H STUB FAIRING BRACKET P/N 6701R10371-2 IAW CRJ SRM
Part: PANEL — CRACKED · airframe 39,450 hrs · 36,470 cycles
PANEL 141AL AND141BL CRACKED (C-CHECK) REMOVED AND INSTALLED NEW SERVICEABLE PANELS IAW SRM .
Part: WINDOW SHADE — MISSING (EMERGENCY EXIT) · airframe 39,450 hrs · 36,470 cycles
RH EMERGENCY EXIT WINDOW SHADE MISSING AND OUTER REVEAL BROKEN. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED RH EMERGENCY EXIT WINDOW SHADE AND OUTER REVEAL IAW AMM.
Part: PIN — CRACKED (WINDOW) · airframe 39,450 hrs · 36,470 cycles
PANELS 832BL, 832BR, 832EL,AND 832ER LATCH PIN WINDOW ARE CRACKED. REMOVED AND REPLACED LATCH PIN WINDOWS IAW SRM.
Part: STRIKER — DAMAGED (PAX DOOR SEAL) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR CUTOUT AFT SEAL STRIKER DAMAGED AT FS 349, UPPER POSITION. (C-CHECK) RO:12/24/2019COMPLIED WITH MAJOR REPAIR OF PAX DOOR CUT OUT AFT SEAL STRIKER DAMAGE AT F.S. 349 IAW BOMBARDIER REO SKYWEST TASK CARD MAJOR REPAIR FORM 337 ATTACHED AND WEIGH AND BALANCE NOT EFFECTED
Part: FITTING — CHAFED (BS 349) · airframe 39,450 hrs · 36,470 cycles
PAX DOOR CUTOUT - AFT ROLLER FITTING CHAFED AT FS 349 UPPER POSITION. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED AFT ROLLER FITTING CHAFED AT FS 349 UPPER POSITION.IAW AMM.
Part: COVER — CRACKED (WINDOW) · airframe 39,450 hrs · 36,470 cycles
PANEL 271ALW HAS CRACKED WINDOW COVER REMOVED AND REPLACED 271ALW REVEAL IAN CMM 25-23-02.
Part: TRACK — BROKEN (WINDOW SHADE) · airframe 39,450 hrs · 36,470 cycles
PANEL 252CLW HAS A BROKEN SHADE TRACK. BONDED THE SHADE TRACK BRACKET IAW SRM.
Part: SPLICE PLATE — CORRODED (RT NACELLE) · airframe 39,450 hrs · 36,470 cycles
TOP OF RH PYLON AT F.S. 742.0 HAS CORROSION ON SPLICE PLATES (C-CHECK) RO:12/24/2019REMOVED AND REPLACED (2EA) SPLICE PLATES ON TOP OF R/H PYLON AT F.S. 742.0 IAW CRJ200 SRM AND CRJ200 AMM BOND CHECK GOOD OHMMETER
Part: PANEL — CRACKED (NOT REPORTED) · airframe 39,450 hrs · 36,470 cycles
PANEL 261BLW CRACKED. REPLACED THE PANEL.
Part: TRACK — BROKEN (WINDOW SHADE) · airframe 39,450 hrs · 36,470 cycles
PANEL 252DLW HAS BROKEN SHADE TRACK. REPAIRED IAW SRM.
Part: COVER — CRACKED (WINDOW) · airframe 39,450 hrs · 36,470 cycles
PANEL 262GLW HAS A CRACKED WINDOW COVER AND CRACKED SHADE TRACK. REPLACED DAMAGED COMPONENTS IAW CMM 25-23-02.
Part: COVER — CRACKED (WINDOW) · airframe 39,450 hrs · 36,470 cycles
261 FLW HAS A CRACKED WINDOW COVER AND IS GOUGED AT THE BOTTOM AFT FACE OF PANEL. REMOVED AND REPLACED 261FLW REVEAL AND REPAIRED PANEL IAW CMM AND RPM.
Part: COVER — CRACKED (WINDOW) · airframe 39,450 hrs · 36,470 cycles
PANEL 251ALW HAS CRACKED WINDOW COVER SURROUNDING. REMOVED AND REPLACED 251ALW REVEAL IAW CMM.
Part: SKIN — ERODED (LT ENG INLET) · airframe 39,450 hrs · 36,470 cycles
LEFT ENGINE INLET LIP SKIN HAD EROSION DAMAGE. REPAIRED THE LT ENGINE INLET LIP SKIN IAW CMM.
Part: RUB STRIP — DEBONDED (LT AILERON) · airframe 39,450 hrs · 36,470 cycles
OUTBOARD EDGE LEFT AILERON RUBBING BLOCK DISBONDED MEASURING APPROXIMATELY 4". REMOVED AND REPLACED THE LT AILERON RUBBING BLOCK IAW REO 601R-57-61-101 REV E.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 39,450 hrs · 36,470 cycles
FOUND CAPTAIN`S RT SEAT TRACK WITH A RIVET STUCK IN ROLLER. REMOVED RIVET. REPAIRED THE CAPTAIN`S RT SEAT TRACK IAW REO.
Part: SKIN — DENTED (LT WING LE) · airframe 39,450 hrs · 36,470 cycles
DENT ON LT WING L/E PANEL BETWEEN WS 167.465 - 176.408 AND MEASURING 2.75L X 1.5W X 0.089D. COMPLIED WITH A PERMENATE REPAIR OF THE DENT IAW SRM.
Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 39,434 hrs · 36,457 cycles
ON APPROACH TO ORD, APPROXIMATELY 10 SECONDS AFTER SELECTING THE LANDING GEAR DOWN RECEIVED A HYD 3A PUMP CAUTION MESSAGE, APPROXIMATELY 10 SECONDS AFTER THAT RECEIVED A GEAR DISAGREE WARNING MESSAGE, ACCOMPANIED BY A HYD 3 LO PRESS CAUTION MESSAGE. DURING THE PERIOD BETWEEN EXTENSION AND WARNING CA AND FO BOTH OBSERVED A WHOOSHING AND SLIGHT VIBRATION, ABNORMAL FROM A REGULAR EXTENSION. LANDING GEAR POSITIONS WERE LEFT - RED DASHES, NOSE - DOWN AND LOCKED, RIGHT - RED DASHES. DECLARED EMERGENCY AND RAN GEAR DISAGREE QRH, WHICH RESULTED IN THE LANDING GEAR BEING MANUALLY EXTENDED. PROCEEDED TO ALSO RUN THE HYD 3 LO PRESS AND SUBSEQUENT NOSE GEAR DOOR OPEN QRH. LANDED IN ORD SAFELY AND WAS TOWED TO THE GATE BY OPERATIONS DUE TO LACK OF NOSE WHEEL STEERING. (FLT#3128) CLOSED REPLACEMENT OF ACMP 3A, REPLACEMENT OF ACMP 3B, REPLACEMENT OF HYD #3 PRESSURE MANIFOLD FILTER, REPLACEMENT OF CASE DRAIN MANIFOLD FILTER FOR ACMP 3A, REPLACEMENT OF CASE DRAIN MANIFOLD FILTER FOR ACMP 3B, AND REPLACEMENT OF HYD #3 RETURN MANIFOLD FILTER IAW AMM.
Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 39,450 hrs · 36,470 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: NDT REAR PRESS BULKHD FWD FACE PART 4/6 - COMPLY WITH TASK CARD 53-280-607 REAR PRESSURE BULKHEAD WEB FORWARD FACE. NDT REAR PRESS BULKHD FWD FACE PART 4/6 - COMPLY WITH TASK CARD 53-280-607 REAR PRESSURE BULKHEAD WEB FORWARD FACE. FOUND REAR PRESSURE BULKHEAD WEB 2 AREAS HAVE MULTIPLE INDICATIONS NOTED 1) BL0.0 WL132-126 50% FSH & 2) LBL9.50 WL74-75.5 70%FSH BOTH FAILED NDT INSPECTION NO OTHER INDICATIONS NOTED AT THIS TIME.
Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 37,728 hrs · 35,080 cycles
HYDRAULIC SYSTEM A WENT FROM 35% ON CLIMB OUT TO YELLOW DASHES, 0%, ON APPROACH AND LANDING. BOTH 1A AND 1B PUMPS WERE OPERATING DURING THE EVENT. (FLT 3130) FO: 02/28/2019 CLOSED REMOVED AND REPLACED LT ACMP, NR 1 PRESS MANIFOLD FILTER ELEMENT, RETURN MANIFOLD ELEMENT, NR 1 HYD DRAIN MANIFOLD FILER ELEMENTS IAW AMM. LEAK CHECK AND PRESSURE CHECK GOOD.
Earlier reports · 2002–2017 · 177 reports
2017
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 35,042 hrs · 32,417 cycles
AFT CARGO FLOOR SUPPORT, BS 559 -559+10 AT LBL 27. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 569-620) · airframe 35,042 hrs · 32,417 cycles
AFT CARGO FLOOR SUPPORT CORRODED, RBL 27, BS 569 - 620. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 559-564) · airframe 35,042 hrs · 32,417 cycles
AFT CARGO FLOOR SUPPORT CORRODED, BS 559+85 - 564, LBL 43. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 559-569) · airframe 35,042 hrs · 32,417 cycles
AFT CARGO FLOOR SUPPORT CORRODED, RBL 9, BS 559+80 - 569. REPAIRED THE FLOOR SUPPORT IAW SRM.
Part: HINGE — GOUGED (PAX DOOR) · airframe 35,042 hrs · 32,417 cycles
PAX DOOR HINGE HALF HAS GOUGED. REMOVED AND INSTALLED A NEW DOOR HINGE IAW SRM.
2016
Part: BULKHEAD — CRACKED (BS 202) · airframe 33,682 hrs · 31,022 cycles
BS 202.75 BULKHEAD CRACKED AT PILOTS BRAKE CONTROL PUSH PULL THROUGH POINT. REPAIRED THE BULKHEAD IAW REO 601R-53-11-653 REV C, REO601R-53-11-2976, REO 601R-53-11-2977, SRM 51-26-00 AND SRM51-51-11. CLASSIFIED AS A MAJOR REPAIR.
2015
Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 31,628 hrs · 29,172 cycles
NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R NR 2 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-05. IPC 33-51-04, FIG 1, ITEM 18. OPS CHECK GOOD.
Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT FS 349 FLOORBEAM AND RBL40. EVALUATED CORROSION AT FS 349.00 AND 349.00 CROSS MEMBER BEAM, REMOVED 1 NUTPLATE IAW SRM 51-21-06. INSTALLED 1 NUTPLATE AT 349 CROSS MEMBER BEAM IAW SRM 51-45-00.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 550AB, LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 550AB CUTOUT IAW SRM 51-21-06. RECIEVED & COMPLIED WITH ECTC EO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 640BB, LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 640BB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC REO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 510AB LOWER WING PLANK ACCESS HOLE LAND HAS CORROSION. REMOVED CORROSION FROM FUEL ACCESS PANEL 510AB IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC EO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 550HB, LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 550HB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC REO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 510 BB LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 510BB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC REO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 540BB LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 540AB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC EO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 640EB, LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 640EB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC REO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 550DB, LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 550DB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC EO 600-57-81.
Part: ACCESS PANEL — CORRODED (WING) · airframe 31,253 hrs · 28,828 cycles
PANEL 540BB LOWER WING PLANK ACCESS HOLE LAND CORRODED. REMOVED CORROSION FROM FUEL ACCESS PANEL 540BB CUTOUT IAW SRM 51-21-06. RECEIVED & COMPLIED WITH ECTC EO 600-57-81.
Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT FS 574-621, LBL 40 FLOOR SUPPORT HAS SURFACE CORROSION AROUND SCREW HOLES. REMOVED CORROSION FROM NUTPLATE HOLES BETWEEN FS 574-621, LT FLOOR SILL IAW SRM 51-21-06. UPON FURTHER EVALUATION SILL AT FS 574-621 + LBL 40 IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. COMPLIED WITH EC/TC REO 601R-53-00-526 & GREO 601R-53-00-526, REV.
Part: STRUCTURE — CORRODED (BS 605-621) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT 621-605.00 & RBL 40 SILL. REMOVED CORROSION AT FS 621-605, RBL 40 SILL IAW 51-21-06 SRM. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-523.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT BS 559+48 - 559, 64LBL 40 FLOOR SUPPORT. REMOVED CORROSION FROM LT FLOOR SILL BETWEEN FS 559.48 AND 559.64 IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF SILL IAW BSC NDT MANUAL SEC 4.3. MIN. REMAINING THICKNESS IS .056" ORIGINAL IS .063". REMOVED IS .007". PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT.1, 51-20-06, NO INDICATIONS NOTED AT THIS TIME. UPON FURTHER INVESTIGATION, FOUND FLOOR SILL TO BE OUT OF LIMITS IAW SRM 53-00-000. COMPLIED WITH EC/TC REO 601R 53-00-026 AND GREO 601R 53-00-526, REV.
Part: FRAME — CORRODED (BS 605) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT 605.00 AND FROM 26L-26R BOTH FWD & AFT SIDES OF FRAME. BEGAN REMOVAL OF CORROSION REF SRM 51-21-06 DAMAGE IS OUT OF LIMITS REF SRM 53-00-00. FABRICATED SPLICE ANGLES 4 & 5 IAW REO DWG 601R-53-61-5559, REV. COMPLIED WITH REO 601R-53-61-5559, REV A. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-61-5559, REV B. COMPLIED WITH REO 601R-53-61-5559. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-61-5559, REV C.
Part: STRINGER — CORRODED (BS 611) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT FS 611 ON STR 27. REMOVED CORROSION FROM STR 27 BETWEEN FS 605 AND 621 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. RECEIVED AND COMPLIED WITH ECTC REO 601R 53-61-5563. RECEIVED AND COMPLIED WITH RGO 601R 53-61-5563.
Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT 364 - 394, RBL9 ON SEAT TRACK. EVALUATED SEAT RAIL AT RS364.00, RBL9-FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL AT FS 364.00-394.00 RBL9 IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT RAIL FS 364.00-394.00, RBL9 IAW REO 601R 53-00-485. INSTALLED NEW FABRICATED SEAT RAIL AT FS 364.00-394.00, RBL9 IAW AMM 53-01-11-400-802. RECEIVED AND COMPLIED WITH ECTC 601R 53-00-485. FABRICATED SEAT RAILS IAW 601R 53-00-485, REV A.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,253 hrs · 28,828 cycles
CRACKED FLOORBEAM CLIP FOUND AT INBD FS 280.00 AND INBD & OTBD LBL9. REMOVED 2 EA CLIPS AT FS 280, LBL9 INBD AND OTBD IAW SRM 51-42-20. INSTALLED 1 EA NEW CLIP AT BS 280, LBL 9, INBD IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2825, REV B AND INSTALLED LT OTBD CLIP IAW SRM 51-42-21. RECEIVED AND COMPLIED WITH ECTC 601R-53-2826.
Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND AT 394 - 409+96 + LBL9 ON SEAT TRACK. EVALUATED SEAT RAIL AT 394.00-409.00 LBL9, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL AT 394.00-409.00, LBL9 IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT RAIL AT FS 394.00-409.00, LBL9 IAW REO 601R 53-00-485. INSTALLED NEW FABRICATED SEAT RAIL AT FS 394.00-409.00, LBL9 IAW AMM 53-01-11-400-802. RECEIVED AND COMPLIED WITH ECTC REO 601R 53-00-485, FABRICATED SEAT RAIL IAW CREO 601R 53-00-485, REV A.
Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND ON SEAT RAIL AT FS 364 - 394, LBL 9. EVALUATED SEAT RAIL AT FS 364.00-394.00, LBL9 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL AT FS634.00-394.00 LBL9 IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT RAIL AT FL 364.00-394.00 AT LBL9 IAW REO 601R 53-00-485. INSTALLED NEW FABRICATED SEAT RAIL FS 364.00-394.00, LBL9 IAW AMM 53-01-11-400-802. RECEIVED AND FABRICATED SEAT RAILS IAW GREO 601R 53-00-485, REV A.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND ON INTERCOSTAL BETWEEN FS 364.00-349.00 AND STR RT, BOTH SIDES. REMOVED RIVETS ON INTERCOSTAL FLANGE TO FS 364.00 AND INTERCOSTAL ATTACHING CLIP TO FS349.00, AND RIVETS ON BOTTOM FLANGE OF INTERCOSTAL IAW SRM 51-42-06-00. OLD INTERCOSTAL WAS CORRODED OUT OF LIMITS IAW SRM 53-00-00. INSTALLED NEW ATTACH CLIP IAW SRM 51-42-06 AND SRM 51-42-21.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 31,253 hrs · 28,828 cycles
CORROSION FOUND ON INTERCOSTAL BETWEEN FS 364.00-349.00 AND STG 26R-26L. REMOVED RIVETS IN ATTACHING CLIP AND FRAME ALSO RIVETS IN BOTTOM FLANGE OF INTERCOSTAL AND REMOVED THE INTERCOSTAL IAW SRM 51-52-06-00. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & REINSTALLED GUSSET PLATE.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,253 hrs · 28,828 cycles
CRACKED FLOORBEAM CLIP FOUND ON 280.00 AND RBL9 OTBD SIDE. REMOVED FLOORBEAM CLIP AT FS 280, RBL9 OTBD SIDE IAW SRM 51-42-20. COMPLIED WITH REO 601R-53-11-2826, REV B TO REPLACE FLOORBEAM CLIP AT FS 280, RBL 9, OTBD SIDE. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-11-2826.
2014
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 29,584 hrs · 27,302 cycles
EMERGENCY EXIT SIGN AT ROW 8 IS BROKEN. REPLACED THE SIGN COVER IAW AMM 33-51-14.
Part: LIGHT — DAMAGED (EXTERIOR) · airframe 29,465 hrs · 27,181 cycles
RIGHT EXTERIOR EMERGENCY LIGHT ASSY NR 6 LIGHT LENS FWD UPPER SCREW NUT PLATE MISSING. R & R EMERGENCY LIGHT ASSY NR 6 IAW AMM 33-51-21. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,435 hrs · 27,153 cycles
NR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW 33-51-21. OPS CHECKED GOOD.
Part: ENGINE — OVERTEMP (LEFT) · airframe 27,289 hrs · 25,035 cycles
CLIMBING OUT OF 10,000 FEET, LT ENGINE ITT WENT INTO RED RANGE. N2 GAGE AT IDLE "VIBRATION" REMAINED. DECLARED AN EMERGENCY, ACFT RETURNED TO DEPARTURE. PERFORMED BORESCOPE INSPECTION ON LT ENGINE. DETERMINED UNSERVICABLE. ENGINE CHANGED IAW AMM 71-00-00-04.
2013
Part: SKIN — CRACKED (LT WING) · airframe 26,969 hrs · 24,682 cycles
TWO LT LOWER WING PLANKS .3750 FASTENER HOLES, 3RD AND 4TH AFT FROM FWD THAT ARE REMOVED IAW SB 601R-57-046, HAVE INDICATIONS NOTED ON INBD AND AFT SIDES APPROX .600" FROM LOWER SURFACE 70 PERCNET FSH MAX. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-2024.
Part: SKIN — CRACKED (RT WING) · airframe 26,969 hrs · 24,682 cycles
FOUND RT LOWER WING FUEL ACCESS HOLE 650BB INBD LANDING HAS MULTIPLE INDICATIONS NOTED 5.0" IN L X .250" W 50 PERCENT FSH FAILED NDT INSPECTION. C/W ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV K.
Part: SKIN — CRACKED (LT WING) · airframe 26,969 hrs · 24,682 cycles
FOUND LT LOWER WING FUEL ACCESS HOLE 540FB INBD LANDING HAS MULTIPLE INDICATIONS. 2.0" IN L X .250 W, 50 PERCENT FSH FAILED NDT INSPECTION. C/W ECTC EO 6900-57-81 AND C/W IAW REO 601R-57-21-030, REV K.
Part: SKIN — CRACKED (WING) · airframe 26,969 hrs · 24,682 cycles
LOWER WING PLANK RT BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES 60 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-57-21-2022, REV.
Part: FLOOR SUPPORT — CORRODED (BS 473.15 & 461) · airframe 26,969 hrs · 24,682 cycles
LEFT FLOOR SUPPORT HAS CORROSION AT FS 473.15 & 461. REMOVED CORROSION IAW SRM 51-21-06 & REO 601R-53-41-666. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.
Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 26,936 hrs · 24,656 cycles
RIGHT PRESSURE FLOOR SUPPORT HAS AREA OF CORROSION AT FS 513. REMOVED CORROSION IAW SRM 51-21-06 & REO 601R-53-41-666. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.
Part: FLOOR PANEL — CORRODED (BS 559) · airframe 26,969 hrs · 24,682 cycles
RT PRESSURE FLOOR PANEL JUST FORWARD OF BS 559 HAS CORROSION AROUND NUTPLATE HOLE. REMOVED CORROSION IAW REO 601R-53-41-666 & SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666 REV C.
Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 26,969 hrs · 24,682 cycles
FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .5 IN LENGTH. REMOVED SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21. LOCATED FASTENER HOLES IN NEW SERVICEABLE SUPPORT BEAM AFT LOWER ANGLE AND INSTALLED IAW SRM 51-40-11 & 51-42-21.
Part: BULKHEAD WEB — CRACKED (REAR CABIN) · airframe 26,969 hrs · 24,682 cycles
FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION LBL 27.50, WL 130 APPROX .4 INCHES IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION, COMPLIED WITH REO 601R-53-61-1541 AND ECTC REO 601R-53-61-1541.
Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 26,936 hrs · 24,656 cycles
LEFT PRESSURE FLOOR ANGLE HAS AREA OF CORROSION AT BS 513. REPAIRED IAW ECTC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.
Part: POST — CRACKED (BS 409) · airframe 26,936 hrs · 24,656 cycles
FOUND FS 409+128 VERTICAL POST LBL 18, HAS A CRACK INDICATION AT AFT FLANGE RADIUS APPROX .2 INCHES IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED VERT POST ASSY IAW SRM 51-42-06. INSTALLED SERVICEABLE POST ASSY IAW SRM 51-42-06, REO 601R-53-41-889.
Part: POST — CRACKED (BS 409) · airframe 26,936 hrs · 24,656 cycles
FOUND FS 409+128, VERTICAL POST BL 0, RT SIDE HAS A CRACK INDICATION AT AFT FLANGE RADIUS APPROX .4 INCHES IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06 AND 51-42-21. DRILL & LOCATED NEW SERVICEABLE POST ASSY. INSTALLED POST ASSY IAW SRM 51-42-06 AND REO 601R-53-41-889.
Part: ATTACH FITTING — CRACKED (LT NACELLE) · airframe 26,936 hrs · 24,656 cycles
LEFT ENGINE FRONT FRAME AFT HUB ATTACH FLANGE CRACKED AT BOLT HOLE ABOVE AGB MOUNT AT 9 O'CLOCK POSITION OF ENGINE. C/W ECTC CF34-3 ENG CHANGE. RECEIVED ALL APPLICABLE PARTS CERTIFICATION PAPERWORK PERTAINING TO LT ENG REPLACEMENT FROM STORES DEPT.
Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 26,936 hrs · 24,656 cycles
AFT PRESSURE BULKHEAD HAS ISOLATOR CRACKED. REMOVED ISOLATOR IAW SRM 51-42-06. INSTALLED NEW ISOLATOR IAW SRM 51-42-06.
Part: ANGLE — CRACKED (BS 484) · airframe 26,936 hrs · 24,656 cycles
LEFT FS 484 FLOORBEAM REPAIR ANGLE CRACKED AT LBL 36.0. REMOVED CRACKED ANGLE IAW SRM 51-42-06. REPLACED ANGLE IAW REO 601R-53-41-059 AND W/O 312243.
Part: ANGLE — CRACKED (BS 484) · airframe 26,936 hrs · 24,656 cycles
RT FS 484 FLOOR SUPPORT REPAIR ANGLE CRACKED AT RBL 36.0. COMPLIED WITH EO CL600-2B19-53-I00449.
Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 26,936 hrs · 24,656 cycles
LEFT FS 409+128 VERTICAL BEAM AT LBL 27 SHOWS VISUAL SIGNS OF A CRACK ON INBD SIDE AT BOTTOM RIVET. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056 REV F. REPAIRED VERTICAL BEAM IAW REO 601R-53-41-056, REV F, DATED 9-2-11.
Part: LIGHT — BROKEN (CABIN) · airframe 26,936 hrs · 24,656 cycles
EXIT FLOORLIGHT ON BOTTOM OF THE ENTRY WARDROBE IS BROKEN. R & R FLOODLIGHT IAW MM 33-51-19-000-801/400-801. PERFORMED SUCCESSFUL OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,394 hrs · 23,180 cycles
INTERIOR CEILING EMERGENCY LIGHT OUT AT ROW 10. R & R LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.
2012
Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 24,392 hrs · 22,142 cycles
HYD SYS 3 INDICATED 20 PERCENT, SELECTED HANDLE DOWN, RECEIVED NOSE GEAR GROUND INDICATION, THEN RECEIVED MAIN DISAGREE MSG. PERFORMED LANDING GEAR MANUAL EXT EMERGENCY DECLARED AS A PRECAUTION. R & R 3A HYD PUMP IAW AMM 29-12-03. R & R NLG SELECTOR VALVE IAW AMM3 32-22-20 JACKED ACFT IAW AMM 07-12-01 PERFORMED GEAR SWING IAW AMM 32-30-00. LEAK AND OPS CK GOOD ACFT OK FOR SVC.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 23,526 hrs · 21,189 cycles
EMERGENCY LIGHT AT SERVICE DOOR IS INOPERATIVE. R & R BULBS. OP'S CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,400 hrs · 21,048 cycles
THE MIDDLE LEFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW THE AMM 33-51-21. OPS CHECKED GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,221 hrs · 20,861 cycles
AFT WING EMERGRNCY LIGHT INOPERATIVE. RELAMPED AFT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
2011
Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 22,987 hrs · 20,593 cycles
PAX DOOR FWD ANCHOR FITTING CRACKED. R & R PAX DOOR FWD ANCHOR FITTING IAW AMM TASK 52-11-17-000-804 & 52-11-17-400-804.
Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 22,987 hrs · 20,593 cycles
LT SIDE SEAT TRACK CORRODED FROM FS 349 TO 409. REMOVED MINOR CORROSION FROM SEAT TRACK, REMOVAL FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-21-49-FIG 1.
Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 22,987 hrs · 20,593 cycles
RT SIDE SEAT TRACK CORRODED AT FS 349.00 TO 409.00. CORROSION OUT OF LIMITS. R & R SEAT TRACK SECTION IAW AMM 53-01-11-000-802 & 53-01-11-400-802.
Part: SILL — CORRODED (BS 574-559) · airframe 22,987 hrs · 20,593 cycles
CARGO COMPARTMENT RT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 574.00+86 AND 559.00+112 AROUND FASTENER HOLES CORRODED. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL REMOVED IS .002". BLEND AREA WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. RESTORED FINISH IAW SRM 51-25-06, 51-26-16, 51-21-11.
Part: SILL — CORRODED (BS 574-589) · airframe 22,987 hrs · 20,593 cycles
CARGO COMPARTMENT RT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 574.00 AND FS 589.00 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3. MIN MATERIAL REMAINING IS .048". BLEND FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-00-00, FIG 102. RESTORED FINISH IAW SRM 51-12-00.
Part: TIE DOWN — CORRODED (BS 559-574) · airframe 22,987 hrs · 20,593 cycles
CARGO BAY RBL 9.00 BETWEEN FS 559.00+85 AND FS 574.00 HAS 2EA TIE DOWN TRACK SEGMENT CORRODED. R & R TIE DOWN TRACKS IAW SRM 51-41-02 AND SRM 53-61-49-00, FIG 2. MINOR REPAIR.
Part: TIE DOWN — CORRODED (BS 559-574) · airframe 22,987 hrs · 20,593 cycles
CARGO BAY LBL 27.00 BETWEEN FS 559.00+80 AND FS 574.00 HAS 1EA TIE DOWN TRACK SEGMENT AND 3 EA TIE DOWN PUCKS CORRODED. REMOVED TIE DOWN IAW AMM 53-01-11-000-802. INSTALLED TIE DOWN IAW AMM 53-01-11-400-802.
Part: ATTACH FITTING — CRACKED (BS 280) · airframe 22,987 hrs · 20,593 cycles
CABIN AREA, AFT BS 280 HAS CRACKED ATTACH FITTING AT STR 3L. REMOVED CRACKED ATTACH FITTING IAW SRM 51-42-21 AND 51-42-06. DRILLED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21, 51-42-06 AND 51-23-00.
Part: TIE DOWN — CORRODED (BS 559) · airframe 22,987 hrs · 20,593 cycles
CARGO COMPARTMENT RBL 27.00 BETWEEN FS 559.00+80 AND FS 559.00+96 HAS 1EA TIE DOWN TRACK SEGMENT CORRODED. R & R TIE DOWN TRACK SEGMENT IAW SRM 51-41-04, 53-61-49.
Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 22,987 hrs · 20,593 cycles
PAX DOOR FWD ANCHOR FITTING CRACKED. R & R WITH NEW ANCHOR FITTING IAW SRM 51-42-21.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 22,996 hrs · 20,605 cycles
PAX DOOR SILL, AFT HAND RAIL STOWAGE CUP FLOOR SUPPORT CLIP CORRODED. R & R CLIP AT PAX DOOR SILL, AFT SIDE IAW SRM 51-42-06. THIS IS A MINOR REPAIR.
Part: SILL — CORRODED (BS 559) · airframe 22,987 hrs · 20,593 cycles
CARGO COMPARTMENT LT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 559.00 AND FS 559.00+112 AROUND FASTENER HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06. PEFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .059" ORIGINAL IS .063" MATERIAL REMOVED IS .004". BLEND AREA WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00 FIG 102, SHEET 2. RESTORED FINISH IAW SRM 51-25-06, 51-26-16, 51-21-11.
Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 22,987 hrs · 20,593 cycles
PAX DOOR AFT ANCHOR FITTING CRACKED. R & R PAX DOOR AFT ANCHOR FITTING IAW AMM TASK 52-11-17-000-804 & 52-11-17-400-804.
Part: SILL — CORRODED (FUSELAGE) · airframe 22,996 hrs · 20,605 cycles
CABIN AREA SERVICE DOOR SILL CORRODED BY AFT THRESHOLD ATTACHMENT BRACKET. REMOVED CORRODED ANGLE AT SERVICE DOOR SILL IAW SRM 51-42-21, CORROSION EXCEEDS ALLOWABLE DAMAGES IAW SRM 53-21-23. LOCATED AND DRILLED NEW SILL SURROUND IAW SRM 51-40-11, INSTALLED IAW SRM 51-41-02.
Part: TIE DOWN — CORRODED (BS 559-621) · airframe 22,987 hrs · 20,593 cycles
CARGO BAY LBL 9.00 BETWEEN FS 559.00+85 AND FS 621.00 HAS 3EA TIE DOWN TRACK SEGMENT AND 2EA TIE DOWN PUCKS CORRODED. R & R CORRODED TIE DOWN TRACKS IAW SRM 51-41-02.
Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 22,987 hrs · 20,593 cycles
WHILE REMOVING FOAM FROM UPPER PART OF AIRSTAIR DOOR, FOUND 3 EA ATTACH FITTINGS CORRODED. R & R 3 EA CORRODED FITTINGS IAW 51-40-11, 51-42-06, & 51-23-00.
Part: ATTACH FITTING — CRACKED (BS 280) · airframe 22,987 hrs · 20,593 cycles
CABIN AREA BS 280 CLIP CRACKED AT RBL 9 OTBD SIDES. REMOVED IAW SRM 51-42-20. FABRICATED IAW REO 601R-53-11-171. INSTALLED IAW SRM 51-42-21 AND REO 601R-53-11-171.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,987 hrs · 20,593 cycles
PAX DOOR DRAG ANGLE CRACKED AT RADIUS JUST ABOVE DOOR ASSIT MOTOR PULLEY BRACKET. . R & R DRAG ANGLE IAW REO 601R-52-11-513.
Part: SKIN — CORRODED (SERVICE DOOR) · airframe 22,987 hrs · 20,593 cycles
SERVICE DOOR LOWER SKIN CORRODED UNDER SCUFF PLATE AFT SECTION. REMOVED CORROSION IAW SRM 51-21-06, STEP 3B, RESTORED FINISH IAW SRM 51-25-01. MINOR REPAIR.
Part: FLT CONTROLS — ERRATIC · airframe 22,872 hrs · 20,460 cycles
ACFT AGGRESSIVELY ROLLED RT WHEN FLAPS SELECTED FROM 30 TO 45. REQUIRED MORE THAN HALF SCALE LWD AILERON TRIM, AT WHICH TIME AILERON CONTROL BECAME ERRATIC DURING NORMAL CORRECTIONS. THERE WAS 'NULL' ZONE AT CENTER OF AILERON TRAVEL AND 'JERKS' WITH SMALL LT AND RT AILERON INPUTS. AUTOPILOT OFF. EMERGENCY DECLARED FL 5300, PERFORMED RIG CHECK OF AILERON CONTROL SYS IAW AMM 27-11-00, PERFORMED OPS TEST OF AILERON CONTROL SYSTEM IAW AMM 27-11-00, PERFORMED OPS TEST OF FLAP CONTROL SYS IAW AMM 27-51-00, CLEANED FLAP UPPER SURFACE AT SEAL POINT TO T/E OF WING SURFACE IAW AMM 51-26-00. PERFORMED FUNCTIONAL TEST OF FLAP FECU IAW AMM 27-51-05, NO DEFECTS NOTED AT THIS TIME.
Part: LINE — LEAKING (FUEL SYSTEM) · airframe 22,724 hrs · 20,286 cycles
STRONG SMELL OF EXHAUST AND OR OIL FUMES IN COCKPIT AND CABIN. R & R APU FUEL SECONDARY MANIFOLD LINES IAW CMM 49-26-39. LEAK AND OPS CHECKED GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,413 hrs · 19,943 cycles
LT MIDDLE EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R LT MIDDLE EXTERNAL EMERGENCY LIGHT BULB. IAW AMM 33-51-21. OP'S CHECKED GOOD.
Part: TERMINAL — ARCED (WINDSHIELD) · airframe 21,829 hrs · 19,275 cycles
F/O WINDSHEILD ARCHING IN FLIGHT COMPLIED WITH QRH PROCEDURES. R & R F/O'S WINDSHEILD IAW AMM 56-11-01. OPS TEST GOOD LEAK CHECK REQUIRED. (CLOSED)
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,414 hrs · 18,779 cycles
RT AFT FUSELAGE EMERGENCY LIGHT INOP. REMOVED THE INOP BULB AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECK GOOD.
2010
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,336 hrs · 18,697 cycles
AFT MOST LT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED AFT MOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED AFT MOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.
Part: PLACARD — MISSING (CABIN) · airframe 20,990 hrs · 18,282 cycles
EXIT PLACARD ON ASD MISSING. INSTALLED EXIT PLACARD ON AIR STAIR DOOR IAW AMM 11-30-00. CLEARED PLACARD REMOVED.
Part: LIGHT — BROKEN (CABIN) · airframe 19,777 hrs · 16,877 cycles
FLOOR EMERGENCY STRIP BROKEN NEAR LAV ON LT. SECURED EMER FLOOR STRIP IAW AMM 25-60-00. (CLOSED)
Part: SILL — CORRODED (ZONE 100) · airframe 19,596 hrs · 16,665 cycles
REPAIRED SILL IAW EC/TC REO 601R-53-21-326 IAW REO 601R-53-21-326 AND COMPLIED WITH EC/TC REO 601R-53-21-1084 IAW REO 601R-53-21-1084. LIGHTNING PORTECTIVE PANEL REQUIRES INSTALL. OK TO INSTALL LIGHTNING STRIKE PANELS. INSTALLED (3) LIGHTNING STRIKE PANELS IAW AMM 53-01-01-410-801.(CLOSED)
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 19,597 hrs · 16,665 cycles
CORROSION FOUND ON FLOOR SUPPORT STRUCTURE JUST FWD AND AFT OF FS 349.00 WL 72.5, RBL 45.0.
2009
Part: ACCESS PANEL — CRACKED (LT WING) · airframe 19,597 hrs · 16,665 cycles
FOUND LT WING LWR PLANK FUEL ACCESS HOLE 540DB HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERENCE OF LANDING 70 PERCENT FSH FAILED NDT INSP, NON-CRITICAL & CRITICAL AREAS. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED FORMS TO STRUCTURES ENGINEERING.
Part: ACCESS PANEL — CRACKED (RT WING) · airframe 19,597 hrs · 16,665 cycles
FOUND RT WING LOWER PLANK FUEL ACCESS HOLE 650CB HAS MULTIPLE INDICATIONS NOTED APPROX 5.0: AREA INBD SIDE NON-CRITICAL 70 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED FORMS TO ENGINEERING.
Part: ACCESS PANEL — CRACKED (LT WING) · airframe 19,597 hrs · 16,665 cycles
FOUND LT WING LWR PLANK FUEL ACCESS HOLE 540CB HAS 2 INDICATIONS NOTED, INBD SIDE NON-CRITICAL AREA OF LANDING 50 PERCENT FSH APPROX 2.0" IN LENGTH, FAILED NDT INSP. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED FORMS TO STRUCTURES ENGINEERING.
Part: BRACKET — CORRODED (BS 349) · airframe 19,597 hrs · 16,665 cycles
FS 349.0 FLOORBEAM JOINT BRACKET HAS CORROSION RT SIDE.
Part: WEB — CRACKED (PAX DOOR) · airframe 19,597 hrs · 16,665 cycles
PAX DOOR FWD WEB IS CRACKED IN RADIUS BETWEEN FIXED STEP AND STEP 832CT. APPROX .200" LONG.
Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,597 hrs · 16,665 cycles
FLOORBEAM AT FS 349, RBL 43 HAS CORROSION .040 DEEP.
Part: POST — CRACKED (BS 409) · airframe 19,597 hrs · 16,665 cycles
FOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. LOCATED AND DRILLED NEW POST IAW SRM 51-40-11. ATTACHED POST TOGETHER IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06, 51-42-22, AND REO 601R-53-41-889.
Part: FRAME — CORRODED (BS 333 S26-27R) · airframe 19,597 hrs · 16,665 cycles
FS 333.0 FRAME CORRODED STR 26R TO STR 27 FWD AND AFT SIDES.
Part: FRAME — CORRODED (BS 349 S26-27L) · airframe 19,597 hrs · 16,665 cycles
FS 349.0 FRAME CORRODED STR 26L TO STR 27 FWD SIDE OF FRAME.
Part: FRAME — CORRODED (BS 310 S26-27R) · airframe 19,597 hrs · 16,665 cycles
FS 310.0 FRAME CORRODED STR 26R TO STR 27 AFT SIDE.
Part: FRAME — CORRODED (BS 319.70 S26R) · airframe 19,597 hrs · 16,665 cycles
FS 319.70 FRAME CORRODED STR 26R AFT SIDE.
Part: STRUCTURE — CORRODED (BS 349) · airframe 19,597 hrs · 16,665 cycles
CORROSION FOUND ON FLOOR SUPPORT STRUCTURE JUST FWD AND AFT OF FS 349.0 WL 73.5, RBL 45.0.
Part: SKIN — CORRODED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011, OPERATION 339/ EXTERIOR SKIN SURFACE FS 559 TO FS 559+32 STRINGER 24L TO 24R HAS CORROSION AROUND FASTENER HOLES AND DRAIN HOLE.
Part: SKIN — CORRODED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011, OPERATION 337/ EXTERIOR SKIN AND SURFACE IS CORRODED FS 559+80 TO FS 559+96 STRINGER 22R TO 23R AROUND FASTENER HOLES.
Part: SKIN — CORRODED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011, OPERATION 338/ EXTERIOR SKIN SURFACE FS 559+32 TO 574.00 HAS SURFACE CORROSION STRINGER 25L TO 25R.
Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 19,597 hrs · 16,665 cycles
JOB 2760015, OPERATION 92/ CARGO DOOR SUPPORT BEAM LWR AFT ANGLE IS CRACKED APPROX 1" IN LENGTH.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
CARGO BAY FLOORBEAM CAP AT LBL27 BETWEEN FS 574.00 AND FS 621.00 HAS MINOR CORROSION AROUND OTBD NUTPLATES.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011, OPERATION 303/ FS 484 RBL 36.0 INTERCOSTAL ANGLE CRACKED IN RADIUS.
Part: PLACARD — MISSING (ECSAPE HATCH) · airframe 19,597 hrs · 16,665 cycles
ALL EXTERIOR PLACARDS ON CREW ESCAPE HATCH MISSING OR UNREADABLE.
Part: WEB — CRACKED (PAX DOOR) · airframe 19,597 hrs · 16,665 cycles
PASSENGER DOOR WEB UNDER TOP FOLDING STEP IS CRACKED AT FWD SIDE APPROX 1.250".
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011 OPERATION 302/FS 484.0 LBL 36.0 INTERCOSTAL ANGLE CRACKED IN RADIUS.
Part: ANGLE — CRACKED (BS 559) · airframe 19,596 hrs · 16,665 cycles
FOUND FS559 HAS 2 INDICATIONS NOTED RT FS559 WEB WL 59.10 APPROX .3" IN LENGTH 70 PERCENT FSH AND LT FS559 LAP ANGLE L8L18 APPROX .2" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. REPAIRED FS 559 FROM LBL 27 TO RBL 27 WEB AND CAP ANGLES IAW REO 601R-53-41-260 REV D. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D. RT SIDE REQUIRES SEALANT, PAINT AND CORROSION PREVENTIVE. PAINTED AND CORROSION PREVENTED RT SIDE IAW REO 601R-53-41-260 PROCEDURE 62 STILL REQUIRES SEALANT. RT REPAIR REQUIRES SEALED. SEALED RT BULKHEAD REPAIR IAW AMM 51-23-00-390-804. (CLOSED)
Part: WEB — CRACKED (PAX DOOR) · airframe 19,597 hrs · 16,665 cycles
JOB 2760011, OPERATION 306/ PASSENGER DOOR AFT WEB IS CRACKED BETWEEN FIXED STEP AND 832CT APPROX .200".
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,597 hrs · 16,665 cycles
FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDING THE LINTEL FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 90 PERCENT FSH FAILED NDT INSP. REPAIRED IAW EC/TC REO 601R-53-61-1230.
Part: WEB — CRACKED (PAX DOOR) · airframe 19,597 hrs · 16,665 cycles
PASSENGER DOOR FWD WEB IS CRACKED BETWEEN STEPS 832AT AND 832BT APPROX .250" LONG.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 19,597 hrs · 16,665 cycles
PHOTOLUMINESCENT TRACK LIGHTING, AFT OF OVER WING INDICATORS, REQUIRES REPLACEMENT DUE TO CRACKED BASES, CRACKED COVERS, AND DETERIORATED CHEVRON MARKINGS. PHOTO STRIPS ARE STILL SERVICEABLE.
Part: INTERCOSTAL — CRACKED (BS 621-625 S14L) · airframe 19,597 hrs · 16,665 cycles
LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED AT RADIUS APPROX 1.0" LONG. REMOVED AND REPLACED INTERCOSTAL AT FS 621 TO FS 625.30, STR 14L WITH A NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-21 11.A AND B(1), AND 9C(1-2).
Part: LIGHT — INOPERATIVE (EXTERIOR EMER) · airframe 19,483 hrs · 16,555 cycles
RT FWD MOST EXTERNAL FUSELAGE EMERGENCY LIGHT INOP.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,460 hrs · 14,558 cycles
AFT SECTION OF OVERHEAD EMERGENCY LIGHT, BOTH CENTER OVERWING EMERGENCY LIGHTS, AND NR 3 EMERGENCY FLOOD LIGHT INOP.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 16,313 hrs · 13,525 cycles
HYD 1 MSG PSI FLUXED AND QTY WENT FROM 70 TO 5%. ENG OPERATED 32 MIN WITH 0 PSI ON HYD SYS 1 (EN ROUTE TO ATL ACFT DIVERTED TO BNA DUE TO MTC, EMERGENCY DECLARED). FLT 4740 DEL 79 MINS. REMOVED AND REPLACED HYD LINE P/N 601R752501 PER CRJ AMM 29-00, NO HELP. REMOVED AND REPLACED HYD LINE 601R75286-37 AND ELBOW ASSY. NO HELP. FOUND HYD LINE 601R75286-61 TO BE CRACKED. REMOVED AND REPLACED HYD LINE IAW CRL AMM 29-00, OPS/LEAK CHECK GOOD. REFER TO LOD 37705-2. (S)
Part: STEP — CRACKED (PAX DOOR) · airframe 16,280 hrs · 13,496 cycles
ASD BOTTOM STEP CRACKED. REMOVED AND REPLACED ASD BOTTOM STEP IAW AMM 52-11-04. OPS CK GOOD. (B)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,726 hrs · 13,024 cycles
LT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,726 hrs · 13,024 cycles
CEILING AFT MOST EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,726 hrs · 13,024 cycles
CEILING EMERGENCY LIGHT 2ND FROM FRONT INOP.
2007
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 15,318 hrs · 12,687 cycles
RT AFT OVERWING EMERGENCY LIGHT IS INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,173 hrs · 12,563 cycles
CENTER EMERGENCY EXIT LIGHT HAS 4 BULBS INOP.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,168 hrs · 12,556 cycles
AAR - PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED.
Part: ANGLE — CORRODED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 FWD ANGLE CORRODED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00399. REMOVED AND LOCATED NEW ANGLE P/N 600-34017-351 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED ANGLE IAW CRJ 200 SRM 51-42-06. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. 14212.
Part: ANGLE — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
AAR-1049, FS 280 LBL 27 O/B ANGLE CRACKED. RESOLVED ON W/O: 75509 TASKCARD: N/R-00333, REMOVED DAMAGED ANGLE FROM FS 280 LBL 27. FS 280 LBL 27 O/B CLIP ANGLE WAS REPLACED ON W/C 1000/0050 PER REO 601R-53-11-1290.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 15,168 hrs · 12,556 cycles
FLOOR SUPPORT AFT OF CARGO DOOR HAS CORROSION.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 RBL 36 I/B ANGLE IS CRACKED.
Part: ANGLE — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 LBL 27 ANGLE CRACKED OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00249. REMOVED AND FABRICATED ANGLE CLIP FOR FS 280LBL 20 OB SIDE IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. INSTALLED PANEL REF 409A IAW CRJ 200 SRM 51-42-13, USING CR3552-4-B AND 4-7 RIVETS.
Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 15,168 hrs · 12,556 cycles
LEFT WING CENTER L/E INBOARD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED ATTACH BRACKET WITH SERVICEABLE BRACKET PN 600-12045-11 IAW CRJ MM 20-21-00.
Part: STRUCTURE — CORRODED (BS 349) · airframe 15,168 hrs · 12,556 cycles
PAX DOOR CUTOUT FRAME FS 349.00 HAS CORROSION. REMOVED MINOR SURFACE CORROSION FROM FWD BRACKET. IAW CRJ SRM 51-21-06. ASSEMBLED BRACKETS TO ANGLES REPLACING CORRODED PART.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 AFT ANGLE CRACKED O/B OF LBL 9 AND RBL 9. CUT AWAY DAMAGED SECTION OF FS280 AFT ANGLE IAW REO 601R-53-11-136. PERFORMED LPI PER NDTM 51-20-08 ON LT & RT CUT LINES TO ENSURE DAMAGE REMOVAL IAW REO 601R-53-11-136 (NO DEFECTS NOTED AT THIS TIME). FABRICATED REPAIR FILLER ANGLE FROM P/N 600-34017-595 AND SPLICE ANGLE IAW REO 601R-53-11-136. OK TO ALODINE PRIME AND TOPCOAT. APPLIED FINISH IAW CRJ 200 SRM 51-21-16. OK TO INSTALL. INSTALLED REPAIR FILLER ANGLE, AND SPLICE ANGLE IAW REO 601R-53-11-136. OK TO TOPCOAT FASTENERS . APPLIED TOPCOAT TO FASTENERS AND REPAIRED AREA IAW CRJ 200 SRM 51-25-16. COMPILED WITH EC/TC EO 600-53-91.
Part: ANGLE — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 RBL 9 ANGLES CRACKED IB AND OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00248). REMOVED 280 RBL 9 CRACKED ANGLE CLIPS I/B AND O/B. FABRICATED SERVICEABLE CLIP ANGLES. REFER TO FORM 412 IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOPCOAT FASTENERS APPLIED TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. INSTALLED DRIP TRAY (REF 409A) IAW CRJ 200 SRM 51-42-13 USING CR 3552-4-2.
Part: ANGLE — CRACKED (BS 280) · airframe 15,168 hrs · 12,556 cycles
FS 280 LBL 9 ANGLES CRACKED I/B AND O/B. FS 280LBL 9 O/B CLIP ANGLE WAS REPLACED PER REO 601R-53-21-787.
Part: ANGLE — CRACKED (BS 625) · airframe 15,168 hrs · 12,556 cycles
LT OBLIQUE ANGLE ON FS 625 CRACKED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00281. REMOVED CRACKED ANGLE, LOCATED IAW CRJ SRM.
Part: PLACARD — WORN (ESCAPE HATCH) · airframe 15,168 hrs · 12,556 cycles
AAR - ALL PLACARDS ON CREW ESCAPE HATCH EXTERIOR ARE WORN.
Part: FITTING — CRACKED (FUSELAGE) · airframe 15,168 hrs · 12,556 cycles
AAR - O/B 280 CLIP AT LBL 9 ON FLOORBEAM HAS A SUSPECTED CRACK. DUPLICATE, REFER TO W/O: 50229 W/C 1000-0041 FOR CORRECTIVE ACTION. SUPPLEMENTAL - SDR CLOSED 11/27/07.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,952 hrs · 12,377 cycles
CEILING FORWARD MOST EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,673 hrs · 11,399 cycles
RIGHT O/W EXTERIOR EMERGENCY AFT LIGHT INOP.
2006
Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 12,843 hrs · 10,772 cycles
SMOKE DETECTOR IN LAV, WILL NOT TEST (LAVATORY SMOKE DETECTION SYSTEM).
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,749 hrs · 10,705 cycles
RIGHT AFT OVERWING EMERGENCY LIGHT BULB BURNED OUT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,749 hrs · 10,705 cycles
LEFT AFT OVERWING EMERGENCY LIGHT BULB BURNED OUT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,661 hrs · 10,632 cycles
LEFT FUSELAGE EXTERIOR, FWD EMERGENGY LIGHT INOP.
Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 11,789 hrs · 9,959 cycles
879 ON TO, A/C HIT A RUBBER RUNWAY PATCH WITH NLG, AFTER TO RECD GEAR DISAGREE, FOUND TORQ LINKS DISC. A/C RETURNED TO SDF AFTER T/O. DELCARED AN EMERGENCY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,659 hrs · 9,826 cycles
AC ESS BUSS CAUTION INTERMITTENTLY WITH EMERGENCY LIGHTS ILLUMINATING INTERMITTENTLY IN THE ARM POSITION.
Part: SIGN — INOPERATIVE (CABIN) · airframe 11,614 hrs · 9,789 cycles
CEILING EXIT SIGN ABOVE LOW 8 OUTSIDE LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,395 hrs · 9,607 cycles
EMERGENCY ESCAPE PATH LIGHTING FAILS OPS CHECK.
Part: CONNECTOR — BROKEN (CABIN) · airframe 11,394 hrs · 9,606 cycles
EMERGENCY FLOOR LIGHT STRIP CONNECTOR 2ND FROM THE FRONT, ON THE FLOOR IS BROKEN.
Part: CONNECTOR — BROKEN (CABIN) · airframe 11,395 hrs · 9,607 cycles
EMERGENCY FLOOR LIGHT STRIP CONNECTOR 2ND FROM THE FRONT ON THE FLOOR IS BROKEN.
Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 11,380 hrs · 9,591 cycles
PAX DOOR FWD AND AFT ANCHOR FITTINGS CRACKED. REMOVED AND REPLACED AFT FITTING, 601R380741-3, AFT LEVER 601R319741-1 AND BEARING M81934/2-10A016 IAW CRJ AMM 52-11-17. REMOVED AND REPLACED FWD FITTING 601R380742-3 IAW CRJ AMM 52-11-17. INSTALLED FWD LEVER 601R319741-2 AND BEARINGS M81934/2-10A016 IAW (CLOSED).
Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 11,380 hrs · 9,591 cycles
RANRC 256. PAX DOOR AFT CLEAT HAS CORROSION.
Part: CLIP — CRACKED (FUSELAGE) · airframe 11,380 hrs · 9,591 cycles
RANRC 198. RT OB FS 484.0 CLIP CRACKED.
Part: CLIP — CRACKED (FUSELAGE) · airframe 11,380 hrs · 9,591 cycles
RANRC 197. LT IB F.S. 484.0 CLIP CRACKED.
Part: CLIP — CRACKED (FUSELAGE) · airframe 11,380 hrs · 9,591 cycles
LT O/B BS 484 CLIP CRACKED. PERFORMED FLUORESCENT INSP ON LT OTBD F.S. 484.00 LBL 36.0 CUT-LINE AND CLIP. NO DEFECTS FOUND PER CRJ NDTM 51-20-08. REMOVED CRACKED CLIP AT LT O/B 484 FABRICATED NEW SERVICEABLE CLIP USING .063 2024-T3 P.O. 3580-1. ALODINED, PRIMED & PAINTED IAW C. (CLOSED)
Part: CLIP — CRACKED (FUSELAGE) · airframe 11,380 hrs · 9,591 cycles
RANRC 198. RT OB FS 484.0 CLIP CRACKED.
Part: CLIP — CRACKED (BS 484) · airframe 11,380 hrs · 9,591 cycles
RT I/B CLIP CRACKED AT F.S. 484. REMOVED CRACKED CLIP AT RT I/ B BS 484 FABRICATED NEW SERVICEABLE CLIP USING .063 2024-T3 PO 3580. ALODINED, PRIMED AND PAINTED IAW CRJ SRM 51-21-11 AND 51-25-00, INSTALLED CLIP ALL WORK DONE IAW REO 601R-53-41-059.(CLOSED)
Part: SILL — CRACKED (BS 589) · airframe 11,380 hrs · 9,591 cycles
CLIP UNDER CARGO DOOR SILL IS CRACKED AT FS 589, REMOVED CLIP AND DUPLICATED IAW CRJ SRM 53-61-23, AND 51-24-21. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CRJ SRM 51-21-11, 51-25-06, AND 51-25-16. OK TO INSTALL. INSTALLED CLIP IAW CRJ SRM 51-42-06 AND 51-42-21. (CLOSED)
Part: RIB — CRACKED · airframe 11,380 hrs · 9,591 cycles
RT BATT RIB CRACKED. REPAIRED RT BATT RIB IAW R.E.O. 601R-57-51-046 (CLOSED)
Part: HINGE — DAMAGED (PAX DOOR) · airframe 11,380 hrs · 9,591 cycles
RANRC 173. HINGE CORRODED BEYOND LIMITS ON PAX DOOR STEP 832ET. REMOVED UNSERVICEABLE HINGE AND INSTALLED NEW HINGE IAW CRJ AMM 52-11-04. (CLOSED)
Part: STEP — CRACKED (AIR STAIR DOOR) · airframe 11,377 hrs · 9,589 cycles
ASD 3RD STEP FROM TOP FWD AND AFT SIDE SKIN CRACKED.
Part: WARNING MESSAGE — ACTIVATED · airframe 11,174 hrs · 9,427 cycles
AC ESS BUSS AND TRANSFER FAIL AND EMERGENCY LIGHTS ARE ON AND SYNOPTIC PAGE SHOWING ADG DEPLOYED AND CAPT VISUALLY VERIFIED ADG IS NOT DEPLOYED, HAD CAPT INSPECT C/B'S AND NO C/B'S ARE POPPED.
Part: HANDLE — CRACKED (FUSELAGE)
DURING A HANGAR INSPECTION, THE PASSENGER DOOR EXTERNAL HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXTERNAL HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2005
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING A HANGAR INSPECTION IN BTR, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: STEP — SEPARATED (DOOR)
DURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE SEPARATED AT THE ATTACHED STAY ROD BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: LAMP — BURNED OUT (CABIN)
DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: CONNECTOR — LOOSE (ENGINE)
DURING CLIMB-OUT FROM ATL-PHF, THE CREW RECEIVED A LT 14TH STAGE DUCT OVERHEAT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE FOUND A LOOSE CONNECTION ON THE LEFT 14TH STAGE BLEED AIR DUCT LOOP AND TIGHTENED THE LOOSE TERMINAL. MAINTENANCE RAN THE ENGINE AT MAX POWER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: CONNECTOR — DIRTY (LT MLG)
DURING APPROACH, UPON GEAR EXTENSION THE CREW RECEIVED A LT MAIN GEAR DISAGREE MESSAGE WITH AN ASSOCIATED (GEAR DISAGREE) EICAS WARNING. THE CREW INITIATED A CLIMB TO PATTERN ALTITUDE TO RUN THE CHECK LISTS AND THEN HEARD A THUD FOLLOWED BY THE LT MLG COMING DOWN AND LOCKING, ALONG WITH THE GEAR DISAGREEMENT AND ASSOCIATED WARNINGS EXTINGUISHING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE CLEANED THE CONNECTOR PLUGS ON THE UPLOCK AND DOWNLOCK SENSORS AND ALSO PERFORMED SEVERAL GEAR EXTENSIONS AND RETRACTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2004
Part: INTERCOSTAL — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, RBL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 484, RBL 36 IAW ASA EO 600-53-0202. (M)
Part: SUPPORT BEAM — CRACKED (RT ENGINE)
DURING A C-CHECK IN MCN, THE RT ENGINE SUPPORT BEAM AT BL 36.20 INBOARD FORWARD CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD AND OUTBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD AND OUTBOARD CLIPS. (M)
Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)
DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD IAW SRM 51-41-06. (M)
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)
Part: SUPPORT BEAM — CRACKED (ENGINE)
DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT IAW ASA EO 600-53-0070. (M)
Part: ANCHOR FITTING — CRACKED (PAX DOOR)
DURING A C-CHECK IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (M)
Part: ANCHOR FITTING — CRACKED (PAX DOOR)
DURING A C-CHECK IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M)
2003
Part: LAMP — INOPERATIVE (LT OVERWING)
FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE LT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR OVEWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2002
Part: LIGHT — INOPERATIVE (EXTERIOR)
FLT 4792 - DURING GROUND INSPECTION AT DFW, AN EXTERIOR LEFT SIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR LEFT SIDE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)