N508AE
Registered owner: AMERICAN AIRLINES INC, TX (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.
237 reports on file, 2003-09-19 – 2025-12-11.
Part: TRANSDUCER — UNSERVICEABLE (ZONE 700) · airframe 49,902 hrs · 38,149 cycles
ANTI - SKID INBD CAUTION MSG ON APPROACH AND IB GND SPLR FAULT STATUS. REMOVED AND REPLACED RT INBD WHEEL SPEED TRANSDUCER IAW 32-44-01-000/400-801-A01. NO DEFECTS NOTED. OPS CHECKED GOOD.
Part: BALLAST — FAILED (ZONE 200) · airframe 49,129 hrs · 37,500 cycles
CABIN CREW REPORTS ELECTRICAL/CIRCUITY SMELL IN THE AFT CABIN AT THE LAST FIVE ROWS. GPU ATTACHED. APU ON. PACKS ON. RECRIC FANS ON. NO LOW PRESS AIR ATTACHED. NO FUELER ACTIVITY PRESENT./ PERFORMED TROUBLESHOOTING IAW CRJ700 FIM 21-22-00-810-806. FOUND TOP SIDEWALL BALLAST ABOVE SEAT 19AC TO BE SOURCE OF THE SMELL. REMOVED AND REPLACED SIDEWALL LIGHT BALLAST ROW 19AC IAW CRJ700 AMM 33-21-09-000/400-801-A01. OPS CHECK GOOD.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
GUSSET AT FS349 AND STRINGER 25L IS CORRODED CORRECTIVE ACTION: INSTALLED NEW GUSSET AT FS349 AND STRINGER 25L IAW CRJ700 SRM 51-42-21-001-001-A01. SH670-32072-1"
Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH INBD FLAP VANE ACTUATOR AT FLS102.9 FWD TRUNNION IS CORRODED CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 102.9 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
DISCREPANCY: FOUND L/H SLAT TRACK 3-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1855 REV-- DATED 2024-11-29. CC670-12081-7
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FS319 BETWEEN STGR25L & 25R FOUND TO BE CORRODED IN MULTIPLE LOCATIONS ON ATTACH FLANGE. CORRECTIVE ACTION: INSTALLED COMPLETE FRAME LOWER SEGMENT PN: SH670-31355-1S FS319 BETWEEN STGR21L & 23R IAW CRJ700 SRM 51-42-06-001-001-A01 SH670-31355-1S
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
DISCREPANCY: FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1856 REV-- DATED 2024-12-02. CC670-12070-3PE
Part: TRUNNION — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"RH OUTBD FLAP W.S. 102.9 AFT TRUNNION HAS CORROSION DAMAGE REQUIRES REPAIR CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 120.9 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21"
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
ANTENNA INNER DOUBLER AT STGR 27 BETWEEN FS 295 AND FS 310 FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
ROUND L/H SLAT TRACK 2-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED LH SLAT TRACK 2-1 IAW MHIRJ REO 670-57-42-1864 REV -- DATED 2024-12-03 CC670-12040-3PE
Part: SLAT TRACK — WORN (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON RH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1857 REV-- DATED 2024-12-02. CC670-12070-3PE
Part: SLAT TRACK — WORN (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 3-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. PERFORMED MAJOR REPAIR ON RH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1854 REV-- (P-1) DATED 2024-12-02. CC670-12090-3PE
Part: STRINGER — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
STRINGER CLIP AT F.S. 985.00, STRINGER 19R IS CORRODED. REMOVED DAMAGED CLIP. FABRICATED AND INSTALLED NEW SERVICEABLE CLIP (P/N MM670-36485-004) I.A.W. CRJ700 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 AND DWG. NO. MM670-36485 MM670-36485-004.
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1856 REV-- DATED 2024-12-02.
Part: SEAT TRACK — ELONGATED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL MOUNTING EXTRUSION HOLES ELONGATED AND PART DENTED DURING REMOVAL OF FASTENERS. REPAIRED LH SIDE SEAT RAIL MOUNTING STRUCTURE BETWEEN FS 741.00 AND 763.00 BY INSTALLING A FREEZE PLUG AND FABRICATING AND INSTALLING REPAIR EXTRUSION IAW MHIRJ REO 670-53-41-713 REV A DATED 2025-03-18. SH670-37522-1
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: REPAIRED AND REPLACED WITH NEW FLOOR BEAM LBL27 FS1000-1069 P/N MM670-35302-035 IAW SRM 53-00-41-201-001-A01 MM670-35302-035
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
" FOUND L/H SLAT TRACK 2-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1870 REV--(P1) DATED 2024-12-03. CC670-12051-9
Part: DOUBLER — CORRODED (ZONE 800) · airframe 48,423 hrs · 36,906 cycles
PAX DOOR STEP PANEL ASSEMBLY (832AT) HAS (3) EACH CRACKS, (3) EACH DENTS WITH ONE EXTENDING INTO THE INTERIOR CENTER RIB, A BENT MOUNTING LUG, AND SPOTS OF CORROSION THROUGHOUT REQUIRING EVAL CORRECTIVE ACTION: REMOVED AND REPLACED NEW SERVICEABLE PAX DOOR STEP ASSEMBLY (832AT) P/N# 601R317076-7 IAW CRJ-700 AMM TASK 52-11-04-000-802 (CONFIG A01) AND TASK 52-11-04-400-802 (CONFIG A01) 601R317076-7
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
DISCREPANCY: FOUND L/H SLAT TRACK 3-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1855 REV-- DATED 2024-11-29. CC670-12081-7
Part: LAP JOINT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH LONGITUDINAL LAP JOINT CORRODED AT STRINGER 20L BETWEEN FS280 AND FS295 CORRECTIVE ACTION: REMOVED CORROSION, PERFORMED NDT AND TREATED AFFECTED AREAS IAW MHIRJ REO 670-53-21-2516 REV.-- DATED 2024-11-27 DRWG SH670-31708
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1856 REV-- DATED 2024-12-02. CC670-12070-3PE
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
PASSENGER DOOR FWD FLOOR CLOSING FITTING AT FS314 IS CORRODED. CORRECTIVE ACTION: REMOVED PASSENGER DOOR FWD FLOOR CLOSING FITTING IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND DEBURRED PASSENGER DOOR FWD FLOOR CLOSING FITTING IAW CRJ700 SRM51-40-11-001-001-A01. INSTALLED PASSENGER DOOR FWD FLOOR CLOSING FITTING PN: SH670-31840-3S IAW CRJ700 SRM 51-42-06-001-001-A01 SH670-31840-3S
Part: TRUNNION — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH OUTBD FLAP W.S. 140.4 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 140.0 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21
Part: TRUNNION — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
FOUND 4EA. TRUNNION BODIES CORRODED ON R/H FLS 24, 65, 102, AND FLS 140 THAT REQUIRE FABRICATION. CORRECTIVE ACTION: FABRICATED 4EA TRUNNION BODIES AT R/H FLS 24.00, 65.50, 102.90 AND 140.40 AS REQUIRED USING 7475-T7351 PO# 5-50407 IAW STEPS 1-3 OF MHIRJ SNIEO 601R14261 IDENTIFIER S21. PERFORMED LPI OF 4 FABRICATED TRUNNION BODIES IAW MHIRJ EO 601R14261 S 21 STEP 4. NO INDICATIONS NOTED AT THIS TIME. PRIMED 4EA NEWLY FABRICATED TRUNNION BODIES IAW MHIRJ SNIEO 601R14261 INDENTIFIER S21 STEP 5. IDENTIFIED EACH NEW TRUNNION BODY 601R14261-S2101 USING INDELIBLE INK IAW MHIRJ SNIEO 601R14261 INDENTIFIER S21 STEP 6. PERFORMED REMAINING STEPS OF MHIRJ SNIEO 601R14261 IDENTIFIER 21. 601R14261-S2101
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
DISCREPANCY: FOUND L/H SLAT TRACK 1-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED LH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-1867 REV -- DATED 2024-12-03 CC670-12030-3PE
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1856 REV-- DATED 2024-12-02.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
AVIONICS BAY DOOR SURROUND INTERCOSTAL 26L BETWEEN F.S 394 AND FS409 IS CORRODED SH670-32075-3
Part: INTERCOSTAL — CHAFED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
STR 9R INTERCOSTAL BETWEEN FS 1144 - FS 1162 HAS CHAFE DAMAGE. PERFORMED A MAJOR REPAIR TO CHAFE DAMAGE ON INTERCOSTAL BETWEEN FS1144.00-FS1162.00, STGR 9R (DEVIATION TO GENERIC REO 670-53-61-292, REV. -E) IAW MHIRJ REO 670-53-61-2437 REV. -- DATED 2024-12-24. SEE SHEET 2 OF REO FOR ADDITIONAL AIRWORTHINESS LIMITATIONS. REFERENCE MHIRJ BARCODE ID: HN00208522 SERIAL NUMBER: 00808 FOR WORK PERFORMED. MM670-36537-012"
Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 1-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. REPAIRED RH SLAT TRACK 1-2 IAW MHIRJ REO 670-57-42-1858 REV -- DATED 2025-02-28 CC670-12021-9
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"LBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: FOUND LBL 9 FLOOR BEAM BETWEEN FS 1000 & FS1069 TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-61-43-101-001-A01. REPAIR REQUIRED. PERFORMED REPAIR IAW CRJ-700 SRM 53-00-41-201-001-A01. S6283 EXTRUSION"
Part: STRINGER — DAMAGED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
STRINGER 7R IS DAMAGED BETWEEN FS 1144 AND FS 1162. CORRECTIVE ACTION: REPAIRED STRINGER IAW BOMBARDIER REO 670-53-61-292 REV E DATED 2017-01-11. MM670-35119-002
Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
WD CARGO DOOR SILL, LOWER AFT JOINT PLATE IS CORRODED. (FS 581) CORRECTIVE ACTION::REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. â DATED 2024-12-18. RWG SH670-33793-3
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
STGR 21L INTERCOSTAL BETWEEN FS310 AND FS333 CORRODED ON BOTH SIDES OF INTERCOSTAL. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. SH670-31822-1S
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
UPON PERFORMING TO_53-079-001-23 REV ORIGINAL DATED 1/25/23 ON STEP (8) CORROSION WAS OBSERVED EXTENDING FROM THE REMOVED FASTENER HOLES IN THE RH FS797.00 AFT OB REMOVED FASTENER HOLES (2) REQUIRING ENGINEERING. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER IAW CRJ 700 SRM 51-24-16-001-001-A01 AND REO 670-53-41-703, REV --(P1), DATED 2024-12-03. COMPLIED WITH REO 670-53-41-703, REV --(P1), DATED 2024-12-03.- REPAIR TO AFT PRESSURE SILL DECK AT FS 797.00, RHS. SH690-36116-1"
Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
WD CARGO DOOR SILL, LOWER AFT JOINT PLATE IS CORRODED. (FS 581) CORRECTIVE ACTION::REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. â DATED 2024-12-18. RWG SH670-33793-3
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
DURING REMOVAL OF L/H SIDE SEAT RAIL MOUNTING EXTRUSION 1EA. HOLE LOCATION AT FS 752.50 JUST BELOW STRG 15L WAS ELONGATED IN UNDERLYING STRUCTURE (LOWER FRAME SECTOR P/N SH670-35522-11) AND REQUIRES REPAIR. CORRECTIVE ACTION: PERFORMED A MAJOR REPAIR TO GOUGE DAMAGE AND ELONGATED HOLE ON LWR FRAME SECTOR AT FS752.50, LHS BY COMPLYING WITH MHIRJ REO 670-53-41-707 REV-DATED 2024-12-22. SEE SHEET 2 OF REO FOR ADDITIONAL AIRWORTHINESS LIMITATIONS. SH670-35522-5
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
RH WINDSHIELD SIDE POST CRACKED APPROX. 4" DOWN FROM TOP AND 1.5" LONG AT 100% FSH. FAILING NDT CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE WINDSHIELD POST P/N 601R33223-2 IAW CRJ700 SRM 51-42-21-001-001-A01. 601R33223-2
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
STRINGER 27 IS CORRODED BETWEEN FS280 AND FS295.CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. SH670-31642-1S
Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH INBD FLAP VANE ACTUATOR AT FLS140.4 FWD TRUNNION IS CORRODED. CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 140.4 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
PANEL 542AZ SUPPORT ANGLE IN LH MLG WHEEL WELL IS CORRODED. REMOVED AND REPLACED LH MLG ANGLE PN CC670-10338-1
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 1-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED LH SLAT TRACK 1-2 IAW MHIRJ REO 670-57-42-1851 REV -- DATED 2025-02-24 CC670-12021-9
Part: FRAME — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
FS295 FRAME LOWER ELEMENT AND WEB CORRODED FROM STGR 20L TO 22L. CORRECTIVE ACTION: FS295 FROM STGR 20L TO 22L FOUND TO BE OUT OF LIMITS PER NOTE 1: DAMAGE IS ALLOWED ONLY IN ONE ELEMENT AT A GIVEN CROSS-SECTION. REMOVED DAMAGE AT ONE ELEMENT MUST NOT OVERLAP WITH REMOVED DAMAGE AT ANOTHER ELEMENT IAW CRJ700 SRM 53-21-06-101-002-A01. COMPLIED WITH CRJ700 SRM 53-00-06-201-006-A01 FOR FRAME SPLICE AT STGR 25L AND LOCATED, DRILLED, AND DEBURRED FS295 FRAME LOWER FRAME SEGMENT FROM STGR19L TO 25L IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED ALL REPAIR PARTS AND FS295 FRAME LOWER FRAME SEGMENT FROM STGR19L TO 25L IAW CRJ700 SRM 53-00-06-201-006-A01 AND 51-42-06-001-001-A01. APPLIED PROTECTIVE FINISHES IAW CRJ700 SRM 51-25-00-001-001-A01. SH670-31353-1S
Part: GUSSET — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
GUSSET AT FS 295 CONNECTING TO STGR 21L FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED GUSSET IAW CRJ700 SRM 51-42-06-001-001-A0. FABRICATED, LOCATED, DRILLED, AND DEBURRED GUSSET PN:SH670-32605-2 FROM S6144-13 IAW CRJ700 SRM 51-40-11-001-001-A01 & 51-24-36-001-001-A01 PER BOMBARDIER DWG SH670-32605. INSTALLED FABRICATED GUSSET IAW CRJ700 SRM 51-42-06-001-001-A01. APPLIED PROTECTIVE FINISHES IAW CRJ700 SRM 51-25-00-001-001-A01.SH670-32605-2
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,423 hrs · 36,906 cycles
L/H SIDE SEAT REAL EXTRUSION REINFORCEMENT STRAP REQUIRES REPLACEMENT. COMPLETE SNIEO SH670-37532-S01 IN ITS ENTIRETY. FABRICATE NEW REINFORCING STRAP P/N: SH670-37532-S0101 SAME AS ORIGINAL STRAP P/N: SH670-37532-1. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ SNIEO SH670-37532 IDENTIFIER S01. SH670-37532-1
Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 48,423 hrs · 36,906 cycles
"STRINGER CLIP AT F.S. 985.00, STRINGER 19R IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED CLIP. FABRICATED AND INSTALLED NEW SERVICEABLE CLIP (P/N MM670-36485-004) I.A.W. CRJ700 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 AND DWG. NO. MM670-36485 MM670-36485-004"
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"LBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: FOUND LBL 9 FLOOR BEAM BETWEEN FS 1000 & FS1069 TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-61-43-101-001-A01. REPAIR REQUIRED. PERFORMED REPAIR IAW CRJ-700 SRM 53-00-41-201-001-A01. S6283 EXTRUSION"
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 1-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: REPAIRED LH SLAT TRACK 1-1 MHIRJ REO 670-57-42-1862 REV-- DATED 2025-02-24 CC670-12010-5
Part: TRUNNION — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH INBD FLAP W.S. 65.5 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 65.5 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
DISCREPANCY: F.S. 295 BETWEEN STGR 26L & 26R PREVIOUS REPAIR IS CORRODED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1015 AND FS 1051.
Part: WEB — CRACKED (ZONE 800) · airframe 48,423 hrs · 36,906 cycles
" PAX DOOR AFT STAIR WEB IS CRACKED. REMOVED AND REPLACED STAIR WEB IAW CRJ-700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. 601R317071-11"
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
PANEL 642AZ SUPPORT ANGLE IN RH MLG WHEEL WELL IS CORRODED. REMOVED AND REPLACED RH MLG ANGLE PN CC670-10338-2
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
AVIONICS BAY DOOR SURROUND INTERCOSTAL 27L BETWEEN F.S 349 AND FS364 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL I.A.W. CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. SH670-32075-3
Part: SEAT TRACK — ELONGATED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL MOUNTING EXTRUSION HOLES ELONGATED AND PART DENTED DURING REMOVAL OF FASTENERS. PART REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED, FABRICATED LEFT SIDE SEAT RAIL EXTRUSION, AND INSTALLED FABRICATED SEAT RAIL EXTRUSION PN SH670-37522-1 IAW MHIRJ REO 670-53-41-713 REV-A DATED 2025-03-18. DUE TO HAVING 2 MAJOR REPAIRS ON ONE CARD, 2 SEPARATE CARDS WERE GENERATED FOR WORK PERFORMED IAW THE REO AND SNIEO. REFERENCE BARCODE HN00223125 FOR WORK PERFORMED IAW REO 670-53-41-713REV-A DATED: 2025-03-18 AND REFERENCE BARCODE HN00223129 FOR WORK PERFORMED IAW SNIEO SH670-37532 S01. SH670-37522-1/SH670-37532-1
Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,423 hrs · 36,906 cycles
FOUND L/H SLAT TRACK 3-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1853 REV-- (P-1) DATED 2024-12-02. CC670-12090-3PE
Part: CRADLE — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"R/H INBD FLAP W.S. 65.5 CRADLE ASSY HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: RECEIVED SERVICEABLE RH WS 65.5 CRADLE ASSEMBLY PN CC670-14301-9. REFERENCE BARCODE HR483812 FOR INSTALL. CC670-14301-9"
Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 2-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON RH SLAT TRACK 2-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1865 REV-- DATED 2024-12-03 CC670-12040-3PE
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
STGR 21L BETWEEN FS280 AND FS295 FOUND TO BE CORRODE IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: STGR 21L BETWEEN FS 280 AND FS295 REQUIRES REPLACEMENT DUE TO BEING IN A NO DAMAGE ALLOWED ZONE IAW CRJ700 SRM 53-21-03-101-002-A01. LOCATED, DRILLED, AND DEBURRED NEW STGR 21L PN: SH670-31209-1S BETWEEN FS 280 AND FS333 IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED STGR 21L PN: SH670-31209-1S BETWEEN FS280 AND FS333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. APPLIED PROTECTIVE FINISHES IAW CRJ700 SRM 51-25-00-001-001-A01.. SH670-31209-1S
Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
L/H I/B FLAP VANE ACUTATOR FWD TRUNNION AT STATION LS 24.0 IS CORRODED.CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 24.0 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
STRINGER SPLICE 19R AT FS333 AND ATTACHED GROUND STUD CLEAT IS CORRODED CORRECTIVE ACTION: REMOVED DAMAGED STGR 21R SPLICE PN (SH670-31197-1) IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-20-001-001-A01. LOCATED, DRILLED, AND DEBURRED FS 333 STGR 21R SPLICE PN:SH670-31197-1S IAW CRJ700 SRM 51-40-11-001-001-A01. APPLIED PROTECTIVE FINISHES IAW CRJ700 SRM 51-25-00-001-001-A01. SH670-31197-1
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FWD CARGO DOOR SILL, LOWER FWD JOINT PLATE IS CORRODED. (FS 533). REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. â DATED 2024-12-18. DRWG SH670-33793-3"
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
THE AFT CARGO DOOR FLOOR SILL IS CORRODED.
Part: SLAT TRACK — WORN (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 2-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON RH SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1869 REV-- DATED 2024-12-03. CC670-12051-9
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
SERVICE DOOR SURROUND BOTTOM SILL ANGLE IS CORRODED CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE SERVICE DOOR SURROUND, BOTTOM SILL ANGLE (PN: SH670-31996-3S) IAW CRJ 700 SRM 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
WHILE REMOVING SCREWS @ MID CAP ANGLE ITEM 65A PN SH670-31825-5, FOUND MID CAP ANGLE TO BE CORRODED REQUIRES R&R. LOCATED AND DRILLED NEW SERVICEABLE MID CAP ANGLE PN SH670-31825-9S IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE MID CAP ANGLE PN SH670-31825-9S IAW CRJ700 SRM 51-41-02-001-001-A01. SH670-31825-9S
Part: INTERCOSTAL — CORRODED (ZONE 800) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
PAX DOOR INTERCOSTAL AFT DD1 FOUND TO BE CRACKED. REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED PAX DOOR INTERCOSTAL AFT DD1 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED PAX DOOR INTERCOSTAL AFT DD1 NEW SERVICEABLE P/N: 601R31902-318 IAW CRJ700 SRM 51-42-06-001-001-A01 601R31902-318
Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 1-2 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: SLAT TRACK WAS REMOVED AND REPLACED IAW CRJ-700 AMM 27-81-41-400-801-A01. CC670-12010-5
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
STRINGER 25R IS CORRODED BETWEEN FS280 AND FS310. CORRECTIVE ACTION: REMOVED AND REPLACE STRINGER IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 SH670-31212-2U
Part: SLAT TRACK — WORN (ZONE 600) · airframe 48,423 hrs · 36,906 cycles
FOUND R/H SLAT TRACK 2-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. REPAIRED SLAT TRACK IAW MHIRJ REO 670-57-42-1866 REV -- DATED 2024-12-03 CC670-12060-3
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FWD CARGO DOOR SILL, LOWER FWD JOINT PLATE IS CORRODED. (FS 533). REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. â DATED 2024-12-18. DRWG SH670-33793-3"
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R CORRECTIVE ACTION: FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R
Part: DOOR SILL — GOUGED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FWD CARGO DOOR SILL INNER CLOSING SKIN HAS MULTIPLE GOUGES BETWEEN FS 565 AND FS 581. CORRECTIVE ACTION: CUT-OUT DAMAGED SECTION OF INNER SKIN AND REMOVED AND DISCARDED JOINT PLATE. FABRICATED AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-31-981 REV. -- DATED 2024-12-18 SH670-33773-5/SH670-33750
Part: WEB — CRACKED (ZONE 800) · airframe 48,423 hrs · 36,906 cycles
PAX DOOR FWD STAIR WEB CRACKED. REMOVED CRACKED WEB. FWD PAX DOOR STAIR WEB HAS BEEN REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01 PN: 601R317071-12S 601R317071-12S"
Part: SEAT TRACK — CORRODED (OZNE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 677 AND FS 708. REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 SRM 51-41-02-001-001-A01 AND 53-00-49-201-002-A01. SH670-36255-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 9 SEAT TRACK F.S. 863-988 HAS CORROSION NEW SEAT TRACK INSTALLED IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A03) SH670-37420-5
Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
TOTAL OF 3 FWD CARGO RETRIEVAL TRACKS HAVE CORROSION. CORRECTIVE ACTION: RECEIVED 2EA FWD CARGO FLOOR TRACKS P/N DSY7058-3 FROM N501BG. REF BARCODE HR00483597 FOR INSTALL. RECEIVED 1 FWD CARGO FLOOR TRACK P/N DSY7058-3 FROM N518AE. REF BARCODE HR00483597 FOR INSTALLATION. DSY7058-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 785.15 AND FS 863. INSTALLED NEW SIDE SEAT RAIL PN SH670-36260-5 IAW CRJ 700 AMM 53-00-49-400-801-A03. SH670-36260-5 "
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 379 AND FS 485 WHILE REMOVING SCREWS @ MID CAP ANGLE ITEM 65A PN SH670-31825-5, FOUND MID CAP ANGLE TO BE CORRODED REQUIRES R&R. WHILE REMOVING SCREWS @ MID CAP ANGLE ITEM 65A PN SH670-31825-5, FOUND MID CAP ANGLE TO BE CORRODED REQUIRES R&R.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 863 AND FS 969. LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 863 AND FS 969. SH670-32234-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 485 AND FS 581. INSTALLED NEW SERICEABLE SEAT TRACK AT LBL 9 FS 485 TO FS 581, P/N SH670-33426-1, IAW CRJ 700 AMM 53-00-49-400-801-A03. SH670-33426-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS485 AND FS572. REMOVED AND REPLACED SEAT RAIL I.A.W. 53-00-49-000/400-801-A03. SH670-32234-3"
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 682. REMOVED AND REPLACED SEAT RAIL I.A.W. CRJ700 AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03 AND T.O. 53-079-002-23 REV.--, DATED 08/04/2023. SH670-33425-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 9 SEAT TRACK F.S. 661-863 HAS CORROSION REPLACED LBL 9 SEAT TRACK F.S. 661-863, PN SH670-35864-3, IAW CRJ 700 AMM 53-00-49-000-801-A03 SH670-35864-3
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH PRESSURE FLOOR SILL ANGLE IS CORRODED BETWEEN FS 761.85 AND FS 785.15.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 682. REMOVED AND REPLACED SEAT RAIL I.A.W. CRJ700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03. SH670-33425-3
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
DENT IN FUSELAGE SKIN AT F.S.1020 BETWEEN STRINGERS 20L AND 21L. CORRECTIVE ACTION: REPAIRED DENT IN FUSELAGE SKIN AT FS1020 BETWEEN STGR21L - 20L,- COMPLIED WITH REO 670-53-61-2429-REV --(P2), DATE 2024-12-31. MM670-35005-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 27 SEAT TRACK F.S. 364-485 HAS CORROSION CORRECTIVE ACTION: REPLACED LBL 27 SEAT TRACK FS 364-485, PN SH690-32127-3. REMOVAL IAW CRJ 700 AMM 53-00-49-000-801-A03. INSTALLED IAW CRJ 700 AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 27 SEAT TRACK F.S. 581-661 HAS CORROSION SH670-33463-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RBL 27 SEAT TRACK F.S. 909-977 HAS CORROSION INSTALLED NEW SEAT TRACK (P/N:SH670-37413-3) IN RBL27 F.S.909.00 TO 977.00 IAW CRJ700 AMM TASK 53-00-49-400-801(CONFIG A03). PAINTED NEW SEAT TRACK IAW T.O. 53-079-002-23 ISSUE DATE 08/04/23 REV N/A. SH670-37413-"
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 572 AND FS 677. REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A03 SH670-32234-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 708 AND FS 761.85. REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A03. SH670-37509-1 SH670-37509-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 863 AND FS 969. SH670-37543-3
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
FS477.40 TO FS691.32 BELOW WL72.00 (ADF ANTENNA FUSELAGE SKIN LIGHTLY CORRODED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 677 AND FS 708. CORRECTIVE ACTION: EVALUATED CORROSION AT STGR 15L BETWEEN FS 677 AND FS 708 FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-41-49-101-001-A01. FABRICATED NEW SERVICEABLE SEAT TRACK P/N SH670-36255-3 IAW CRJ 700 SRM TASK 53-00-49-201-002-A01 AND RECEIVED SERVICEABLE SEAT TRACK FROM PAINT. INSTALLED NEW SERVICEABLE SEAT RAIL P/N SH670-36255-3 IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A03).
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 485 AND FS 581. REMOVED AND REPLACED SEAT RAIL I.A.W. CRJ700 AMM 53-00-49-000/400-801-A03. SH670-33426-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 485 AND FS 572. INSTALLED NEW LH SEAT RAIL P/N SH670-32234-3 AT STGR 15L BTW FS 485 - FS 572 IAW CRJ-700 AMM 53-00-49-400-801 (CONFIG A03)
Part: ELEVATOR — CORRODED (ZONE 300) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
EA23-C7-55-0445 PERM REPAIR BEFORE 48,428.02 FH - L/H ELEVATOR ASSY WITHIN 2,041.57 FHâS (BEFORE 48,428.02 FH) FROM REV. IR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RRECTIVE ACTION: PERFORMED EA23-C7-55-0445 PERMANENT REPAIR BEFORE 48,428.02 FH 0N L/H ELEVATOR ASSY WITHIN 2,041.57 FH TRAILING EDGE LOWER SKIN BETWEEN RIB 13 - RIB 15; IAW, MHIRJ REO 670-55-21-161 REV --(P1) DATED 2024-11-13. ELEVATOR P/N: AV670-24100-009, S/N: AVHS 7055. AV670-24100-009
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"RBL 9 SEAT TRACK F.S. 350-485 HAS CORROSION CORRECTIVE ACTION: INSTALLED NEW RBL 9 SEAT TRACK ON F.S.350.00 TO F.S.485.00 IAW CRJ700 AMM TASK 53-00-49-400-801 (CONFIG A03). PAINTED NEW SEAT TRACK IAW T.O. 53-079-002-23 ISSUE DATE 08/04/23 REV N/A. SH670-32159-1"
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 27 SEAT TRACK F.S. 923-977 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ-700 AMM 53-00-49-400-801-A03 AND SRM 53-00-49-201-002-A01. SH670-37412-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RBL 9 SEAT TRACK F.S. 661-863 HAS CORROSION REPLACED RBL 9 SEAT TRACK F.S. 661-863, PN SH670-35864-3, IAW CRJ 700 AMM 53-00-49-000-801-A03 SH670-35864-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
LBL 9 SEAT TRACK F.S. 374-485 HAS CORROSION DAMAGED SEAT TRACK REMOVED IAW CRJ 700 AMM 53-00-49-000-801 (CONFIG A03) NEW SEAT TRACK INSTALLED IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A03) SH670-32249-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 708 AND FS 761.85 INSTALLED NEW RH SIDE SEAT RAIL LOCATED AT F.S.708-F.S.761.85 IAW CRJ 700 AMM 53-00-49-400-801-A03. SH670-37509-1
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 379 AND FS 485. REMOVED AND REPLACED SEAT RAIL I.A.W. CRJ700 AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03 AND T.O. 53-079-002-23 REC.--, DATED 08/04/2023. SH670-32233-3
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,423 hrs · 36,906 cycles
"RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 572 AND FS 677. REMOVED AND REPLACED SEAT RAIL I.A.W. CRJ700 AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03 AND T.O. 53-079-002-23 REV.--, DATED 08/04/2023. SH670-33558-3 "
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00203618 DISCREPANCY: PASSENGER DOOR LOWER SILL KICKPLATE ANGLE CORRODED AT FS 330.00 CORRECTIVE ACTION: REMOVED KICKPLATE ANGLE SH670-31875-3 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE KICKPLATE ANGLE P/N SH670-31875-3 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
Part: ACTUATOR — CORRODED (ZONE 500) · airframe 47,650 hrs · 37,455 cycles
HN00203060 SN: 00541 DISCREPANCY: LH IB FLAP VANE ACTUATOR AT FLS24.00 UPPER TRUNNION HAS CORROSION; ACTUATOR CRADLE HAS DAMAGE IN RIG BOLT AREA CORRECTIVE ACTION: LOCATED AND MACHINED 3EA HOLES IN NEW SERVICEABLE LH IV FLAP VANE ACTUATOR ROD AT FLS 24.00 IAW CRJ 700 SRM 51-40-11-001-001--A01 REFERENCING DWG CC670-14303 FOR SIZES AND DIMENSIONS. REFER TO HR00493692 FOR INSTALL OF LH IB FLAP VANE ACTUATOR ASSY AT FLS24.00 (PN-CC670-14300-9-01 SN-PR1937)
Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00202827 DISCREPANCY: PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 FWD SIDE FOUND CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 FWD SIDE IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 FWD P/N#601R318086-1 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01
Part: SKIN — CORRODED (ZONE 800) · airframe 47,650 hrs · 37,455 cycles
HN00202845 SN: 00536 DISCREPANCY: PAX DOOR INNER SKIN FOUND TO BE CORRODED. CORRECTIVE ACTION: REPAIRED: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER SKIN PN 601R318024-7 IAW CRJ700 SRM 51-40-11-001-001-A01REFERENCE HN 00200644 FOR INSTALLATION OF INNER SKIN.
Part: ACTUATOR — CORRODED (ZONE 600) · airframe 47,650 hrs · 37,455 cycles
HN00203076 SN: 00545 DISCREPANCY: RH IB FLAP VANE ACTUATOR AT FLS65.50 UPPER TRUNNION BODY HAS CORROSION CORRECTIVE ACTION: LOCATED AND MACHINED 3EA HOLES IN NEW SERVICEABLE RH IB FLAP VANE ACTUATOR ROD AT FLS 65.50 IAW CRJ 700 SRM 51-40-11-001-001-A01 REFERENCING DWG CC670-14303 FOR SIZES AND DIMENSIONS. REFER TO HR00493751 FOR INSTALL OF RH IB FLAP VANE ACTUATOR AT FLS65.50
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
FLOOR SEAT TRACK LOCATED AT F.S.985-F.S.1000 RBL 27 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED FLOOR SEAT TRACK LOCATED AT F.S.985-F.S.1000 RBL 27 IAW CRJ 700 AMM 53-00-49-000-802-A06. INSTALLED NEW SERVICEABLE SEAT TRACK PN: BA670-45073-3 AT F.S.985 - F.S.1000 ON RBL 27 IAW CRJ-700 SRM 51-21-11-001-001-A01, 51-23-00-001-001-A01 AND 51-41-04-001-001-A01.
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00203618 DISCREPANCY: PASSENGER DOOR LOWER SILL KICKPLATE ANGLE CORRODED AT FS 330.00 CORRECTIVE ACTION: REMOVED KICKPLATE ANGLE SH670-31875-3 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE KICKPLATE ANGLE P/N SH670-31875-3 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 47,650 hrs · 37,455 cycles
FRAME SECTOR FS 379.00 CORRODED BETWEEN STR 22R AND 23R REMOVED FS 379 FRAME SECTOR IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW FRAME SECTOR PN# SH670-32118-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.
Part: TRUNNION — CORRODED · airframe 47,650 hrs · 37,455 cycles
FOUND 6EA TRUNNION BODIES CORRODED ON L/H FLS 24.00, 65.50, 108 AND R/H FLS 65.50, 108, AND 140 THAT REQUIRE FABRICATION . CORRECTIVE ACTION: 6EA TRUNNION BODIES ON L/H FLS 24.00, 65.50, 108 AND R/H FLS 65.50, 108, AND 140 FLAP VANE ACTUATORS ASSYS WERE REPLACED THEREFOR NO FABRICATED TRUNNION BODIES REQUIRED FOR REPLACEMENT OF L/H FLS 24.00, 65.50, 108 AND R/H FLS 65.50, 108, AND 140 FLAP VANE ACTUATOR ASSYS
Part: STRINGER — CORRODED (ZONE 100) · airframe 47,650 hrs · 37,455 cycles
HN00203616 SN: 00580 DISCREPANCY: STR 22R CORRODED AT FS 319.00 CORRECTIVE ACTION: REMOVED AND INSTALLED NEW STRINGER 22R BETWEEN FS 280 AND FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00202826 DISCREPANCY: PAX DOOR FRAME 338.963 FOUND CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: PAX DOOR FRAME 338.963 SHOULDE BE FRAME 320, REMOVED FRAME 320 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR FRAME FS320 P/N 601R318032-5 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FRAME FS320 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 47,650 hrs · 37,455 cycles
HN00203624 SN: 00587 DISCREPANCY: AVIONICS BAY DOOR SURROUND INTERCOSTAL FS 349.00 TO FS 364.00 STR 27 (L/H) IS CORRODED ON AFT END CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE P/N:(SH670-32075-3S) INTERCOSTAL @ FS 349.00-FS 364.00 STR 27 (L/H) IAW CRJ700 SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01, 51-42-21-001-001-A01, & 51-26-00-001-001-A01
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00203305 SN: 00553 DISCREPANCY: LBL 27.0 FLOOR SUPPORT UPPER SURFACE HAS TWO SPOTS OF CORROSION AROUND NUPLATE HOLES AT FS1028.00 AND FS1036.00 REPAIRED LBL27 FLOOR SUPPORT IAW CRJ 700 SRM 53-00-41-201-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 47,650 hrs · 37,455 cycles
HN00202820 DISCREPANCY: PAX DOOR MID INTERCOSTAL DD6 FOUND CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED INTERCOSTAL DD6 IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD6 MID P/N#601R318057-1 IAW CRJ-700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00202825 DISCREPANCY: PAX DOOR DD4 AFT FOUND TO BE CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD4 AFT P/N 601R31902-317A IAW CRJ-700 SRM TASK 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD4 AFT IAW CRJ-700 SRM TASK 51-42-06-001-001-A01
Part: TRUNNION — CORRODED · airframe 47,650 hrs · 37,455 cycles
FOUND 1EA TRUNNION BODIE CORRODED ON L/H FLS 140.00 THAT REQUIRES FABRICATION CORRECTIVE ACTION: FABRICATED FWD TRUNNION BODY BY COMPLYING WITH MHIRJ SNIEO 601R14261 IDENTIFIER S22 DATED 05-FEBRUARY-25.
Part: MOUNT — CORRODED (ZONE 700) · airframe 47,650 hrs · 37,455 cycles
HN00203615 DISCREPANCY: RBL 16.0 FS 285.00 GALLEY1 MOUNT FITTING CORRODED CORRECTIVE ACTION: REMOVED FITTING AND INSTALLED NEW SERVICEABLE FLOOR FITTING P/N 670-32149-3 IAW CRJ700 51-42-21-001-001-A01
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00203428 SN: 00567 DISCREPANCY: RH FLOOR SILL FS310-319 SHOW SIGNS OF CORROSION IN MULTIPLE AREAS. REMOVED AND INSTALLED P/N SH670-32172-5 SILL/BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00202842 DISCREPANCY: PAX DOOR MID INTERCOSTAL DD2 FOUND CORRODED. REQUIRES REPLACEMENT CORRECTIVE ACTION:LOCATED AND DRILLED UP PAX DOOR MID INTERCOSTAL IAW CRJ-700 SRM 51-40-11-001-001-A01.INSTALLED PAX DOOR MID INTERCOSTAL DD2 P/N# 601R318053-3 IAW CRJ-700 SRM TASK 51-42-21-001-001-A01, AND TASK 51-42-06-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 47,650 hrs · 37,455 cycles
HN00203306 SN: 00554 DISCREPANCY: LBL 9.0 FLOOR SUPPORT UPPER SURFACE HAS LOCALIZED SPOT OF CORROSION AT FS1033.00 REPAIRED LBL 9 FLOOR SUPPORT BY REPLACING SEGMENT BETWEEN F.S. 977 TO F.S.1064 IAW CRJ 700 SRM 53-00-41-201-001-A01 FIG 830.
Earlier reports · 2003–2023 · 113 reports
2023
Part: CIRCUIT BOARD — UNSERVICEABLE (ZONE 100) · airframe 47,011 hrs · 35,674 cycles
BRAKE OVHT WARNING MESSAGE IN FLIGHT / BRAKE OVHT WARNING MESSAGE IN FLIGHT / REMOVED AND REPLACED JB10-PCB3 IAW CRJ700 AMM 24-05-07-000/400-801. OPERATIONAL TEST DONE IAW CRJ700 AMM 24-05-07-710-801-A01 AND FOUND GOOD.
Part: ACM — SMOKE (200) · airframe 47,006 hrs · 35,671 cycles
L PACK AUTO FAIL AND SMOKE IN COCKPIT / REMOVED AND REPLACED LH ACM IAW CRJ 700 AMM 21-51-08-000/400-801. OPS CHECK GOOD.
2022
Part: BLEED VALVE — FAULTED (LT ENGINE) · airframe 46,048 hrs · 34,831 cycles
LEFT ENGINE SURGE CLOSED CAUTION MSG IN FLIGHT. REMOVED AND REPLACED OPERABILITY BLEED VALVE IAW CRJ700 AMM 75-31-01-000/400-801-A01.
Part: DIMMER — ODOR (CABIN LIGHTS) · airframe 45,975 hrs · 34,769 cycles
UPON ARRIVAL TO AIRPLANE THAT WAS NOT POWERED A STRONG CHEMICAL/BURNING SMELL WAS PRESENT. REMOVED AND REPLACED POWER DIMMER UNIT IAW CRJ 700 AMM33-21-09-000/400-801. OPS CHECK GOOD.
Part: SPOILER — FAULT MESSAGE · airframe 45,259 hrs · 34,124 cycles
WHILE ENROUTE TO DCA, CREW RECEICED AN IB FLIGHT SPOILER AND IB SPOILERONS CAUTION MESSAGE. THEY RAN THROUGH THE QRH AND DECIDED TO DIVERT TO IAD. THEY DID DECLARE AN EMERGENCY BUT DID NOT HAVE THE CABIN BRACE. FLIGHT LANDED IN IAD WITHOUT FURTHER INCIDENT. INBD FLT SPOILER AND INBD SPOILERON CAUTION MSGS IN FLIGHT / PERFORMED SYSTEM RESET, MESSAGES CLEARED AND DID NOT RETURN."
Part: HARNESS — UNSERVICEABLE (700) · airframe 44,418 hrs · 33,376 cycles
MULTIPLE BRAKE OVHT WARNINGS IN FLIGHT RAN QRH MESSAGE EXTINGUISHED. DEFERRED RH OB BTMSPER CRJ 700 MEL 32-46-01 CAT C. M FUNCTION C/W BY PLACING HIGH TEMP LACING TAPE OVER CONNECTOR AND ZIPTIE THE CANON PLUG. PLACE PLACARD/STICKER ON SECONDARY EICAS DISPLAY. INSULATION AND CONTINUITY CHECKED GOOD. REMOVED AND REPLACED MLG WOW PROX SENSOR HARNESS IAW CRJ 700 AMM 32-61-05-000/400-803. BITE/OPS TEST OF TEMP MONITORING SYSTEM GOOD.REQUIRES ADJUSTMENTS OF RH OB PROX SENSOR. PREFORMED ADJUSTMENTS OF RH OB PROX SENSOR (WOW) OPS CHECK GOOD. IAW CRJ 700 AMM 32-61-05-820-803."
2021
Part: WINDSHIELD — CRACKED (COCKPIT LEFT) · airframe 42,323 hrs · 31,473 cycles
CAPTAIN REPORTED CRACKS IN THE WINDSHIELD WHILE ENROUTE TO CLT. NO EMERGENCY DECLARED AND FLIGHT LANDED SAFELY IN CLT. MX INSPECTED THE WINDSHIELD AND NOTICED THAT THE CRACKS WERE JUST IN THE OUTSIDE LAMINATE. REMOVED AND REPLACED L/H WINDSHIELD HEATER CONTROLLER IAW CRJ 700 AMM 30-41-06-00-801 AND 30-41-06-400-801.REMOVED AND REPLACED CAPTAINS WINDSHIELD UP TO CLOSEOUT B7. OPS CHECKS STILL MEED COMPLIED WITH AS WELL AS CURE TIME IAW CRJ 700 AMM 56-11-01-000/400-801-A01-PSA.
2019
Part: RETURN LINE — LEAKING (RT ENGINE) · airframe 40,603 hrs · 29,973 cycles
FUEL LEAK UNDER RT ENGINE. FOUND RETURN LINE TO RT ENGINE OBV IS DAMAGED. REMOVED AND REPLACED RT ENGINE OBV FUEL RETURN LINE. IAW AMM 73-21-09-00/400-801-01. LEAK AND OPS CHECKED GOOD.
Part: WEB — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR FWD WEB FOUND TO BE CORRODED. REMOVED SUPPORT ANGLES AND NUTPLATES FROM DAMAGED PAX DOOR FWD WEB IAW CRJ 700 SRM 51-42-06/13/21-001-001-A01 REV 37. LOCATED, DRILLED UP, INSTALLED NUTPLATES & SUPPORT ANGLES ON NEW PAX DOOR FWD WEB PN 601R317071-128 IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06/13/21-001-001-A01 REV 37. . REF MWC 21007211/121 FOR PAX DOOR AFT WEB INSTALLATION AND OPS CHECK OF PAX DOOR. PAX DOOR FWD WEB STEP NUTPLATE HOLES REQUIRE LOCATE/DRILLE AND NUTPLATES REQUIRE INSTALL. LOCATED, DRILLED AND INSTALLED NUTPLATES ONE FWD WEB IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-15-001-001-A01 REV 37 08/15/19 FOR STEP PNLS. REMOVED PAX DOOR FWD COUNTERBALANCE IAW CRJ 700 AMM 52-11-17-000
Part: DOOR FRAME — CORRODED (BS 311) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
FWD PAX DOOR FWD FRAME AT FS 311.75 IS CORRODED ON BOTH SIDES. J.ROY 10/10/19(JW) M/A: 1. REMOVED FWD FRAME PAX DOOR @ 311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01. J.DROZDIK,B.KELLEY 10/17/19 C/A: 1. INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 700 SRM 51-42-06-21-001-001-A01 REV 37 AUG 15,2019. B.GROGG 11/07/19 M/A: 2. N/A C/A: 2. LOCATED AND DRILLED UP NEW PAX DOOR FWD FORMER PN 601R318031-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15,2019. B.GROGG 10/23/19 (11/12/19JW)
Part: FRAME — CRACKED (BS 347) · airframe 40,428 hrs · 29,807 cycles
PAX DOOR FS 347.25 FRAME IS CRACKED BELOW THE SUPPORT WHEEL AND FASTENERS ARE PULLING THROUGH SKIN. REMOVED FRAME PAX DOOR @ FS 347.25 IAW CRJ 700 SRM 51-42-00-001-001-A01. INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 700 SRM 51-42-06-21-001-001-A01 REV37 AUG 15,2019. LOCATED AND DRILLED UP NEW PAX DOOR AFT FORMER PN 601R318034-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15,2019.
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR UPPER FWD INTERCOSTAL DD2 IS CORRODED. REMOVED PAX DOOR INTERCOSTAL DD2 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR UPPER FWD INTERCOSTAL DD2 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37. LOCATED AND DRILLED UP NEW PAX DOOR UPPER FWD INTERCOSTAL DDIA PN 601R318033-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV37 AUG 15/2019.
Part: DOOR FRAME — CRACKED (BS 347) · airframe 40,428 hrs · 29,807 cycles
PAX DOOR FS 347.25 FRAME IS CRACKED BELOW THE SUPPORT WHEEL AND FASTENERS ARE PULLING THROUGH SKIN. J.ROY 10/10/19(JW) M/A: 1. REMOVED FRAME PAX DOOR @ FS 347.25 IAW CRJ 700 SRM 51-42-00-001-001-A01. J.DROZDIK,B.KELLEY 10/17/19 C/A: 1. INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 700 SRM 51-42-06-21-001-001-A01 REV37 AUG 15,2019. B.GROGG 11/07/19 M/A: 2. N/A C/A: 2. LOCATED AND DRILLED UP NEW PAX DOOR AFT FORMER PN 601R318034-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15,2019. B.GROGG 10/22/19 (11/13/19JW)
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR LOWER AFT INTERCOSTAL IS CORRODED. REMOVED PAX DOOR LOWER FWD AFT INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR LOWER AFT INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37. LOCATED AND DRILLED UP NEW PAX DOOR LOWER AFT INTERCOSTAL PN 601R318033-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV37.
Part: FORMER — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR FORMER AT FS 329.41 DD5 AND DD6 IS CORRODED. REMOVED PAX DOOR FORMER AT FS 329.41 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR FORMER AT FS 329.41 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15/2019. LOCATED AND DRILLED UP NEW PAX DOOR FORMER AT FS 329.41 DD5 AND DD6 PN 601R318078-3 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV37.
Part: FRAME — CORRODED (BS 311) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
CORRECTED ID NUMBER. FWD PAX DOOR FWD FRAME AT FS 311.75 IS CORRODED ON BOTH SIDES. REMOVED FWD FRAME PAX DOOR @ 311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 700 SRM 51-42-06-21-001-001-A01 REV 37 AUG 15,2019. LOCATED AND DRILLED UP NEW PAX DOOR FWD FORMER PN 601R318031-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15,2019.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR INTER COSTALS BETWEEN FS 338.963 TO FS 347.25 IS CORRODED 1EA MARKED WITH TAP. REMOVED INTERCOSTAL PAX DOOR @ 338.963 AND FS 347.25 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW INTERCOSTAL IN PAX DOOR AT FS 338.963 FS 347.25 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15/2019. LOCATED AND DRILLED UP NEW PAX DOOR AFT MID INTERCOSTAL PN 601R31902-317 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15/2019.
Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR INNER SKIN IS CORRODED IN VARIOUS LOCATIONS MARKED WITH TAPE. 1. REMOVED NUTPLATES FROM DAMAGED PAX DOOR INNER SKIN IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15,2019. LOCATED AND DRILLED UP NEW INNER SKIN FOR PAX DOOR PN 601R318024-7 AND INSTALLED NUTPLATES ON SKIN IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 37, MWC 2100724/145 FOR PAX DOOR INNER SKIN REMOVAL/INSTALLATION.
Part: COVER — CRACKED (DOOR HINGE) · airframe 40,428 hrs · 29,807 cycles
PAX DOOR AFT HINGE FAIR WG IS CRACKED IN MULTIPLE LOCATIONS AND DELAMINATING. LOCATED, DRILLED UP NE PAX DOOR ANGLE AFT FAIRING PN 601R31895-16 USING STANDARD SHOP PRACTICES. REF MWC 21007211/146 FOR INSTALL OF FAIRING.
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
RH INTERCOSTAL AT STGR 26R BETWEEN FS 349 AND FS 364 HAS MINOR CORROSION. STGR 26R HAS MULTIPLE SPOTS OF FITTING CORROSION FROM FS280-FS364. STGR 26R FROM FS280-364 DAMAGE FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-21-03-101-002-A01 AND 53-21-03-101-006-A01. REMOVED STGR 26R (AFT SECTION,SPLICE, AND FWD SECTION) FROM FS280-364 IAW CRJ 700 SRM 51-42-06-001-001-A01. . LOCATED AND DRILLED NEW SECTIONS (FWD AND AFT) STGR 26R FS280-364 IAW CRJ 700 SRM 51-40-11-001-001-A01. REMOVED STGR CLEATS FROM FS319,333,310 AND 295 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 STGR 26R. REINSTALLED STGR CLEATS FROM FS295,310,319,333 AND 349 IAW CRJ 700 SRM 51-42-06-001-001-A01. REMOVED FRAME SPLICE AT
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR UPPER MID INTERCOSTAL DD1A IS CORRODED. REMOVED PAX DOOR UPPER MID INTERCOSTAL DDIA IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37. INSTALLED NEW PAX DOOR UPPER MID INTERCOSTAL DDIA IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37. LOCATED AND DRILLED UP NEW PAX DOOR UPPER MID INTERCOSTAL DDIA PN 601R318033-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV37.
Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR INNER SKIN IS CORRODED IN VARIOUS LOCATIONS MARKED WITH TAPE. REMOVED NUTPLATES FROM DAMAGED PAX DOOR INNER SKIN IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15,2019. LOCATED AND DRILLED UP NEW INNER SKIN FOR PAX DOOR PN 601R318024-7 AND INSTALLED NUTPLATES ON SKIN IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 37 AUG 15,2019. REF MWC 2100724/145 FOR PAX DOOR INNER SKIN REMOVAL/INSTALLATION.
Part: WEB — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR AFT WEB IS CORRODED. REMOVED SUPPORT ANGLES AND NUTPLATES FROM DAMAGED PAX DOOR AFT WEB IAW CRJ 700 SRM 51-42-06/13/21-001-001-A01 REV 37 LOCATED, DRILLED UP, INSTALLED NUTPLATES & SUPPORT ANGLES ON NEW PAX DOOR AFT WEB PN 601R317071-113 IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06/13/21-001-001-A01 REV 37 08/15/19 REF MWC 21007211/121 FOR PAX DOOR AFT WEB INSTALLATION AND OPS CHECK OF PAX DOOR. PAX DOOR AFT WEB STEP NUTPLATE HOLES REQUIRE LOCATED/DRILLED AND NUTPLATES REQUIRE INSTALL. LOCATED, DRILLED AND INSTALLED NUTPLATES PAX DOOR AFT WEB IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06/15-001-001-A01. REMOVED PAX DOOR AFT COUNTERBALANCE IAW CRJ 700 AMM 52-11-17-000-802 A01 REV 62 08/25
Part: LEVER — CRACKED (PAX DOOR) · airframe 40,428 hrs · 29,807 cycles
PAX DOOR UPPER LEVER ASSY FOR THE PAX DOOR IS CRACKED. INSTALLED LEVER IAW CRJ700/900 SRM 51-42-21-001-001-A01.
Part: STIFFENER — CRACKED · airframe 40,428 hrs · 29,807 cycles
PAX DOOR AFT MOTOR STIFFENER IS CRACKED. REMOVED DAMAGED PAX DOOR AFT MOTOR MOUNT STIFFENER LOCATED DRILLED AND INSTALLED NEW STIFFENER PN 601R317745-7 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 37 AUG 15,2019.
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR INTERCOSTALS BETWEEN FS 323 TO FS 335 3 INTER COSTALS CORRODED FROM THE TOP OF DOOR MARKED WITH TAPE. 10/10/19(JW) M/A: 1. REMOVED INTERCOSTALS PAX DOOR FS 323 TO FS 335 3EA IAW CRJ 700 SRM 51-42-06-001-001-A01. 10/17/19 C/A: 1. INSTALLED 3EA NEW PAX DOOR MID INTERCOSTALS BETWEEN FS 323 FS 335 IAW CRJ 700 SRM 51-42-06 21-001-001-A01 REV 37 AUG 15/2019. 10/31/19 M/A: 2. N/A C/A: 2. LOCATED AND DRILLED UP NEW PAX DOOR MID INTERCOSTALS PNS 601R318056-1 601R318057-1 AND 601R318081-1 IAW CRJ 700 SRM 51-40-11-001-001-A01. REV 37 AUG 15/2019. 10/22/19 (11/05/19JW)
Part: GUSSET — CORRODED (BS 313-323) · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR GUSSET IS CORRODED BETWEEN FS 320 AND FS 323. UPON INVESTIGATION FOUND 1EA ADDITIONAL CLEAT AT FS 313.56 CORRODED REMOVED DAMAGED PAX DOOR CLEATS IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 3 AUG 15/2019. INSTALLED 2EA NEW CLEATS 1EA AT FS 313.56 AND 1EA BETWEEN FS 320 AND 323 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15/2019. LOCATED AND DRILLED UP NEW PAX DOOR CLEATS PN 600-31902-269 2EA IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15/2019.
Part: FRAME — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR FS 320 FRAME IS CORRODED. J.ROY 10/10/19(JW) M/A: 1. REMOVED DAMAGED PAX DOOR FS 320 FRAME IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15/2019. M.FREEMAN 10/21/19 C/A: 1. INSTALLED NEW PAX DOOR FS 320 FRAME IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37 AUG 15/2019. M.FREEMAN 10/31/19 M/A: 2. N/A C/A: 2. LOCATED AND DRILLED UP NEW PAX DOOR FRAME PN 601R318038-3 IAW CRJ 700 SRM 51-40-11-001-001-A01 REV 37 AUG 15/2019. M.FREEMAN 10/22/19 (11/05/19JW)
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 40,428 hrs · 29,807 cycles
PAX DOOR LWR FWD INTERCOSTAL DD5 IS CORRODED. REMOVED PAX DOOR LWR FWD INTERCOSTAL DDS IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 37. INSTALLED SAME SERVICEABLE PAX DOOR LWR FWD INTERCOSTAL DD5 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV37. INTERCOSTAL REQUIRES REPAIR. PERFORMED PERMANENT REPAIR OF MINOR SURFACE CORROSION IAW BSC EO CL 600-2610-52-LO 6259.
Part: COMPUTER — FAILED (FUEL QTY) · airframe 40,026 hrs · 29,458 cycles
ON CLIMB OUT OF CVG, AT FL250, CREW RECEIVED AUTO CROSS FLOW INHIBIT, AND THE LEFT FUEL GAUGE DASHED OUT. THE CREW DID DECLARE AND EMERGENCY WITH ATC. &R FQGC IAW AMM 28-41-22-000/400-801-A01. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,012 hrs · 29,446 cycles
EXIT ROW BOTTOM EMERGENCY LIGHT ONLY COMES ON BREIFLY A/C RIGHT. R&R EMERGENCY BATTERY PACK & CHARGING ASSY IAW CRJ 700 AMM 33-51-17-000/400-802-A01 (CHARGING UNIT) / 33-51-000/400-801 CONFIG A01. OPS CHECK GOOD AT THIS TIME.
Part: ADC — FAILED (NR 2) · airframe 39,663 hrs · 29,133 cycles
UNRELIABLE AIRSPEED INDICATION. THE FLIGHT DIVERTED. DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI TO A GATE UNDER THEIR OWN POWER. R & R THE NR 2 ADC, OPS CHECKED GOOD.
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 38,977 hrs · 28,547 cycles
RT PACK ON DEFERRAL, LT PACK AND RECIRC FAN REMAINED ON WHEN STARTING ENGINES WITH A TAIL WIND WHICH CAUSED A SMOKE SMELL IN THE COCKPIT AND CABIN. AIRCRAFT RTG. PERFORMED ENGINE STARTS, OPS CHECK GOOD. NO SMOKE/FUME SMELL NOTED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,944 hrs · 28,519 cycles
EMERGENCY FLOOD LIGHTS 5 AND 6 AND R/H WING FLOOR LEVEL EXIT SIGN DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK #4 IAW CRK 700 33-51-17-000/400-801 OPS CHECK GOOD
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 38,908 hrs · 28,485 cycles
L/H OVERWING EXIT LOWER EMERGENCY EXIT LIGHT HAS (1) BULB BURNT OUT. INSPECTED L/H OVERWING EXIT LIGHTS AND FOUND ALL BULBS PROPERLY ILLUMINATING IAW CRJ 700 AMM 33-51-00-710-801-A01.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 39,908 hrs · 28,485 cycles
R/H OVERWING EXIT LOWER EMERGENCY EXIT LIGHT HAS (1) BULB BURNT OUT. INSPECTED R/H OVERWING EXIT LIGHTS AND FOUND ALL BULBS PROPERLY ILLUMINATING IAW CRJ 700 AMM 33-51-00-710-801-A01.
2018
Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,255 hrs · 26,963 cycles
EXTERNAL FUSELAGE SKIN HAS 4 AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AT STR 27. REPAIRED IAW ERS-CR-53MR-3293.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 37,255 hrs · 26,963 cycles
LEFT SIDE OF FLOORBEAM ANGLE WAS FOUND CRACKED AT BS 280. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,255 hrs · 26,963 cycles
FLOORBEAM FS280.00 CRACKED JUST LEFT OF COCKPIT ENTRANCE ON THE TOP SURFACE. REMOVED AND REPLACED LT FLOORBEAM AT FS280.00 IAW SRM 53-11-41.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 37,255 hrs · 26,963 cycles
RIGHT LOWER BULKHEAD WEB AT BS 280 WAS CORRODED. REMOVED AND REPLACED THE BULKHEAD WEB IAW SRM 53-11-10-201-004, AND SRM 51-42-06.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,255 hrs · 26,963 cycles
FLOORBEAM FS280.00 CRACKED JUST RIGHT OF COCKPIT ENTRANCE ON THE TOP SIDE. REMOVED AND REPLACED RT FLOORBEAM AT FS280.00 IAW SRM 53-11-41.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 37,255 hrs · 26,963 cycles
RT FLOORBEAM ANGLE IS CRACKED AT BS 280. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.
2017
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,529 hrs · 26,375 cycles
FA #2 FLASHLIGHT LED IS INOP-C/A-REMOVED AND REPLACED FA #2 FLASHLIGHT IAW AMM 25-61-02 OP CK GOOD
Part: SENSOR — FAILED (LT MLG BRAKE) · airframe 35,989 hrs · 25,942 cycles
ON INITIAL CLIMBOUT, BRAKE OVERHEAT WARNING. WITH GEAR DOWN, TEMP DECREASE WITH LATER ERRATIC TEMP INDICATIONS. ERRATIC TEMP INDICATIONS WITH WARNING MESSAGE CONTINUED DURING TAXI IN. REMOVED AND REPLACED NR 4 MLG BRAKE TEMP SENSOR, OPS CHECKED GOOD IAW AMM 32-46-01.
Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 35,150 hrs · 25,276 cycles
LAST 2 CEILING EMERGENCY LIGHTS INOPERATIVE. NR 5 & 6 NOT ILLUMINATED WHEN EMERGENCY LIGHT SWITCH IS ON. SWAPPED EMERGENCY LIGHTS 3 & 4 WITH 5 & 6 IAW AMM 33-51-09, LIGHTS 1-4 OPS CHECKED GOOD, LIGHTS FIVE AND SIX STILL BAD. REPAIRED THE CONNECTOR J360 IAW ESPM 20-33-00. OPS CHECKED GOOD.
Part: SWITCH — MALFUNCTIONED (SPOILERONS) · airframe 34,681 hrs · 24,899 cycles
AFTER TAKEOFF RECIEVED SPOILERON ROLL CAUTION MESSAGE. COMPLIED WITH QRH AND RETURNED TO AIRPORT. MESSAGE POSTED AND CLEARED AGAIN 3-4 TIMES. REMOVED AND REPLACED ROLL DISCONNECT SWITCH IAW MM 27-61-25. OPS CHECKED GOOD.
2016
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,247 hrs · 24,559 cycles
MAIN EXIT EMERGENCY LIGHTS HAS TWO BURNED OUT BULBS. R & R THE BULBS IAW 33-51-05. NO DEFECTS NOTED.
Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 34,131 hrs · 24,475 cycles
EMERGENCY LIGHTS ARE INTERMITTENT FLASHING ON AND OFF WITH BOTH SWITCHES IN ARMED POSITION. REMOVED AND REPLACED RELAY K135 IAW AMM 24-06-11, AND 20-42-00. OPS CHECKED GOOD.
Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 34,103 hrs · 24,449 cycles
NR 1 FA FLASHLIGHT NOT INDICATING A CHARGE WHEN PLACED INTO CHARGER. REMOVED AND REPLACED THE FLASHLIGHT CRADLE AND FLASHLIGHT. OPS CHECKED GOOD. IAW AMM 25-61-02.
Part: QUICK DISCONNECT — LOOSE (MLG BRAKE) · airframe 33,422 hrs · 23,835 cycles
AFTER TOUCHDOWN AND ROLLOUT, NOTICED THAT I HAD TO APPLY MORE BRAKING THAN USUAL. DURING TAXI IN, LT OTBD BRAKING, REGISTER 00, LT INBD BRAKE 08. THE RT INBD BRAKES REGISTERED 05, RT OTBD BRAKES 07. ACFT, DURING ROLLOUT AND BRAKING, PULLS TO THE RIGHT. FOUND NR 1 BRAKE NOT WORKING DUE TO LOOSE QUICK DISCONNECT HYD FITTING AT BRAKE. RESECURED FITTING. PERFORMED OPS CHECK OF BRAKES IAW AMM 32-43-00. OPS CHECK, LEAK CHECK GOOD.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 33,405 hrs · 23,817 cycles
REF TDMI 508T5333 -DENT NR 1 LOCATED BETWEEN STR 18R AND STR 19R, FS1031.00 AND FS1051.30. 1.25" X 0.875" X 0.32MM DENT. DENT NR 2 SAME LOCATION AS DENT NR 1, 4.0" X 0.625" X 0.12 MM. REF LOG PAGE 3947041, ITEM 3. REPAIR COMPLIED WITH IAW ERS-CR-53MR-1844.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,405 hrs · 23,817 cycles
LEFT AND RIGHT ANGLES AT FS 280 AND BL9 ARE CRACKED. INSTALLED LT AND RT ANGLES, T-BRACKETS AT FS 280 AND BL 9 IAW SRM 53-11-41, 51-42-06, 51-42-21.
Part: STEP — CRACKED (PAX DOOR) · airframe 33,405 hrs · 23,817 cycles
PASSENGER DOOR STEPS AFT SIDE SKIN HAS A CRACK AT THE BOTTOM STEP. COMPLIED WITH REPAIR IAW ERS-CR-5200-589.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 33,405 hrs · 23,817 cycles
LEFT JACK FITTING SUPPORT BETWEEN FS 265.00-280.00 IS CORRODED. COMPLETED REPLACEMENT OF LT JACK FITTING SUPPORT IAW SRM 51-42-06.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 33,405 hrs · 23,817 cycles
RIGHT JACK FITTING SUPPORT BETWEEN FS 265.00-280.00 IS CORRODED. COMPLETED REPLACMENT OF RT JACK FITTING SUPPORT IAW SRM 51-42-06.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 33,405 hrs · 23,817 cycles
LEFT AND RIGHT SIDES OF CROSSBEAM AT FS 280.00 EACH HAVE A .7500" CRACK. R & R LT AND RT CROSSBEAM AT FS 280.-00 IAW SRM 51-42-06 AND 51-42-13.
Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 32,466 hrs · 23,104 cycles
DURING TAKEOFF ROLL, BELOW 50 KTS WE RECEIVED A RT PACK AUTO FAIL MSG ON ED 1. A LOW SPEED ABORT AT 68,000 LBS TAKEOFF WEIGHT. THE MSG WENT AWAY AFTER THRUST LEVERS WERE RETURN TO IDLE. DEFERRED CABIN TEMP CONTROL SYS AUTO MODE. M PROCEDURES COMPLIED WITH IAW 21-64.
2015
Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,549 hrs · 22,361 cycles
ENTRANCE COMPARTMENT EMER FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT & HOLDER ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.
Part: ROLLER — DIRTY (CABIN DOOR) · airframe 30,790 hrs · 21,736 cycles
FLIGHT ATTENDANT REPORTS THAT CABIN DOOR IS NOT OPENING & CLOSING AS EASILY AS NORMAL. CLEANED & LUBED CABIN DOOR ROLLERS & SHOOT BOLTS. OPERATIONS CHECKED GOOD IAW AMM 52-11-02.
Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 30,322 hrs · 21,349 cycles
CAPTAINS FLASHLIGHT INOPERATIVE. REPLACE FLASHLIGHT BULB IN CAP IN FLASHLIGHT AS REQUIRED.
Part: RELAY — INOPERATIVE (CABIN) · airframe 30,291 hrs · 21,326 cycles
EMERGENCY LIGHT INOPERATIVE. R & R RELAY K135 OF JB-11. OPERATIONS CHECKED GOOD IAW AMM 24-06-11.
Part: STATUS MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 30,289 hrs · 21,323 cycles
EMERGENCY LIGHTS ON MESSAGE STATUS. RESET, OPS CHECKED GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,277 hrs · 21,315 cycles
ON BOARDING, NOTICED THAT EMER LIGHTS ON MSG, SHOWING WHILE IN ARM POSITION. CYCLED BOTH FLIGHT ATTENDANT SWITCH & COCKPIT SWITCH LIGHTS ALWAYS ON IN THE ARM POSITION. CYCLED CB'S S11, POWER SENSORS, & U3 EMER LIGHT. WITH APU POWERED, EMER TROUBLE SHOT, OPERATIONS CHECKED OK FROM FLIGHT ATTENDANT & COCKPIT SWITCHES IAW AMM TASK 33-51-00-210-802. CONFIG A010 OK FOR SERVICE.
2014
Part: FITTING — CRACKED (FUSELAGE) · airframe 29,212 hrs · 20,497 cycles
FOUND PAX DOOR LINTEL STRINGER 3 CRACKED. REPAIRED IAW SB 670BA-53-040 REV C & REO 670-53-21-493.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,885 hrs · 20,268 cycles
RIGHT AFT EXTERIOR EMER LIGHT FAILS TO ILLUMINATE. R & R LIGHT BULB IN RT AFT EXTERIOR EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-51-15.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,523 hrs · 20,016 cycles
MAIN AVIONICS UNDERFLOOR STRINGER 25RT. BETWEEN FS 295.00 & FS 310.00 IS CORRODED. REPLACED STRINGER IAW SRM 51-42-06.
Part: SHELF — CRACKED (E&E BAY) · airframe 28,523 hrs · 20,016 cycles
RIGHT SIDE OF FWD EQUIP COMPARTMENT SHELF HAS A CRACK AT FS 193. CRACK GOES UNDER THE ADG HAND PUMP & IS APPROX 3/4 INCH IN LENGTH. REPAIRED RT SIDE OF FWD EQUIP COMPARTMENT SHELF IAW ETN CR-53-099.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,523 hrs · 20,016 cycles
MAIN AVIONICS UNDERFLOOR STRINGER 26RT, BETWEEN FS 319.70 & FS 333.00 IS CORRODED. STRINGER 26RT REPAIR BETWEEN FS 319.70 & FS 333.00 IAW ERS-CR-53MR-408.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,523 hrs · 20,016 cycles
LEFT CROSSBEAM ANGLE AT FS 280.00, BL 9.04 IS CRACKED. INSTALLED BRACKET IAW SRM 51-42-06 & 51-42-20.
Part: CONTROL CABLE — FRAYED (RT AILERON) · airframe 28,523 hrs · 20,016 cycles
RIGHT AILERON CABLE IN WW AREA THAT CONNECTS TO AILERON SERVO MOUNT IS FRAYED. R & R CABLE IAW AMM 27-11-00-400-804 & E379813 FOR CABLE TENSION CHECK.
Part: SHELF — CRACKED (E&E BAY) · airframe 28,523 hrs · 20,016 cycles
LEFT SIDE OF FWD EQUIP COMPARTMENT SHELF HAS A CRACK AT FS 193. CRACK IS APPROX 1/8 INCH IN LENGTH. REPAIRED LT SIDE OF FWD EQUIP COMPARTMENT SHELF AT FS 193 IAW ETN CR-53-099.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,523 hrs · 20,016 cycles
RIGHT CROSSBEAM ANGLE AT FS 280.00, BL 9.04 IS CRACKED. INSTALLED BRACKET IAW SRM 51-42-06 & 51-42-20.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,482 hrs · 19,994 cycles
PILOT`S FLASHLIGHT IS INOPERATIVE. R & R PILOT`S FLASHLIGHT IAW CMM 25-60-11, OPERATIONS CHECKED GOOD.
Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 28,320 hrs · 19,888 cycles
GOUGE ON RT LOWER FUSELAGE BETWEEN FS 453.00 - FS 477.40 & STRINGERS 23RT - 26RT IAW LOG PAGE 3541526, ITEM 2. REPAIRED GOUGE IAW ERS-CR-53MR-304.
Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 28,318 hrs · 19,887 cycles
STEERING INOPERATIVE CAUTION MSG EN ROUTE. R & R NLG WIRING HARNESS IAW AMM 20-07-00.
Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 28,304 hrs · 19,878 cycles
AFTER LANDING & CLEARING ROV ON HIGH SPEED GOT EICAS MASTER CAUTION NOSE WHEEL STEERING INOPERATIVE. TRIED TO RECONNECT, UNABLE MULTIPLE REPEAT WRITE UPS, SEE YESTERDAY PG 3541519 NOTIFIED DISPATCH, MOC, OPERATIONS TUGGED INTO GATE. R & R LT NOSE WHEEL PROXIMITY SENSOR HARNESS IAW AMM 32-61-05, OPERATIONS CHECK FAILED NEXT ITEM THIS LOG PG.
Part: ACTUATOR — FAILED (NLG STEERING) · airframe 28,304 hrs · 19,878 cycles
PASSING THROUGH 14,000 FEET, CREW RECEIVED EICAS STEERING INOPERATIVE MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES & CONTACTED SOC & MOC. THE DECISION TO RETURN WAS MADE. THE CAPTAIN DECLARED AN EMERGENCY & ELECTED TO LAND AT JFK DUE TO USE OF LONGER RUNWAY. R & R LT NW STEERING ACTUATOR IAW CRJ 700 AMM 32-52-01, OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 28,195 hrs · 19,809 cycles
FOUR LAMPS ON LT OVERWING FLOOR EXIT SIGN WILL NOT ILLUMINATE. R & R FOUR LAMPS ON LT OVERWING FLOOR EXIT SIGN IAW AMM 33-51-01. OPERATIONS CHECK IAW AMM 33-51-00, OPERATIONS CHECKED GOOD.
Part: STEERING SYS — FAULTED (NLG) · airframe 28,180 hrs · 19,799 cycles
STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT, AFTER LANDING USED RESET PROCEDURE. STEERING FAILED AGAIN WHILE PARKING AT THE GATE. DISCONNECTED & RECONNECTED J1, J2 & J3 ON NOSE WHEEL STEERING ECU IAW AMM 32-51-10. OPERATIONS CHECKED GOOD IAW AMM 32-51-05.
2013
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,476 hrs · 19,326 cycles
F/O FLASHLIGHT DOES NOT WORK. R & R FLASHLIGHT IAW MM 25-61-02. OPS CHECKED GOOD.
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 26,877 hrs · 18,945 cycles
CREW REPORTED THAT AFTER TAKEOFF THE NOSE GEAR DID NOT RETRACT. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. MDC INDICATED "NG CENTERED NR 2 SENSOR/UNREASON-FAR" ADJUSTED PROXIMITY SENSOR PX37 AND PX08 IAW AMM 32-61-05, OPS TEST GOOD. OPS TEST OF LANDING GEAR EXTENSION/RETRACTION SYS GOOD IAW AMM 32-30-00. THE ACFT WAS RETURNED TO SERVICE.
Part: FLASHLIGHT — BROKEN (CABIN) · airframe 26,046 hrs · 18,415 cycles
ON FLIGHT 3744 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT CRADLE IN THE AFT CABIN WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW CRJ AMM25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 25,516 hrs · 18,087 cycles
DURING FLIGHT 3605 THE CREW REPORTED THE NR 1 F/A'S FLASHLIGHT CRADLE DOES NOT HOLD FLASHLIGHT IN PLACE THEREFORE IT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 F/A FLASHLIGHT CRADLE ASSY IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,298 hrs · 17,948 cycles
ON FLIGHT 3761 THE CREW REPORTED, HEARD A LOUD QUICK BANG SOUND AND SAW THE FIRST OFFICERâS OUTER PANE WINDSHIELD HAD CRACKED AT FLIGHT LEVEL 250, NO ICING CONDITIONS. THE CREW IMMEDIATELY DECLARED AN EMERGENCY AND REQUESTED A DESCENT. THE CREW FOLLOWED ALL APPLICABLE CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE FIRST OFFICERâS WINDSHIELD. THE AIRCRAFT WAS RETURNED TO SERVICE.
2012
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 24,521 hrs · 17,469 cycles
DURING 2C CHECK FOUND AFT LOWER WEB OF THE RIGHT BULKHEAD AT FS 280.0 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LOWER WEB IAW STRUCTURAL REPAIR MANUAL 53-11-10. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 24,521 hrs · 17,469 cycles
DURING 2C MAINTENANCE INSPECTION FOUND THE AFT LOWER FACE OF THE LEFT BULKHEAD HAS EVIDENCE OF CORROSION AT FS 280.00. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AFT LOWER FACE OF THE LEFT BULKHEAD IAW CRJ SRM 53-11-10. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SILL — CORRODED (FUSELAGE) · airframe 24,521 hrs · 17,469 cycles
DURING 2C CHECK FOUND RIGHT CABIN OUTBOARD FLOORBOARD SUPPORT FROM FS 280.00 TO THE SERVICE DOOR SILL CUT OUT HAS EVIDENCE OF CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD SERVICE DOOR SILL IAW BOMBARDIER CRJ700 STRUCTUAL REPAIR MANUAL 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 24,521 hrs · 17,469 cycles
DURING 2C MAINTENANCE INSPECTION FOUND CROSSBEAM AT FS 280.00 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CROSSBEAM IAW BOMBARDIER CRJ 700 STRUCTURAL REPAIR MANUAL 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SEAT — DIRTY (COCKPIT) · airframe 24,496 hrs · 17,456 cycles
ON FLIGHT 3802 THE CREW REPORTED A BAD ODOR FROM FORWARD JUMPSEAT (F/A) WHEN SEAT IS IN USE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED SEAT AND SURROUNDING AREAS. COULD NOT DUPLICATE ODOR. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: HYDRAULIC LINE — FAULTY (HYDRAULIC SYS) · airframe 24,462 hrs · 17,433 cycles
ON FLIGHT 3715 THE CREW REPORTED ON DESCENT TO PHL THE HYDRAULIC NR 2 SYSTEM QUANTITY 20%, HYDRAULIC PRESSURE 0. THE CREW RAN THE CHECK LIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN HYDRAULIC PUMP HOSE IAW 29-11-01 AMM. REMOVED AND REPLACED THE NR 2 HYD ENGINE DRIVEN PUMP IAW AMM 29-11-01, THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE NR 2 PRESSURE MANIFOLD FILTER IAW AMM 29-11-09, THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE NR 2 CASE DRAIN FILTER IAW AMM 29-11-40, THE OPERATIONAL CHECK WAS GOOD NO LEAKS NOTED. ELEMENT FILTER PART NUMBERS, AC7031FB, 7593394-002. PUMP HYD ENGINE DRIVEN PART NUMBER 66190-05, SERIAL NUMBER K0053A. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — UNSECURE (CABIN) · airframe 23,715 hrs · 16,943 cycles
ON FLIGHT 3765, THE CREW REPORTED THE EMERGENCY ESCAPE PATH MARKER ON FLOOR NEEDS TO BE RE-SECURED, FORWARD MARKER LEFT AND RIGHT OVERWING EXIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED EMERGENCY ESCAPE PATH MARKER (LEFT AND RIGHT SIDE) ON FLOOR WITH DOUBLE SIDED TAPE IAW CRJ-700 STANDARD MAINTENANCE PRACTICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 23,690 hrs · 16,927 cycles
FLIGHT 3695, CREW REPORTED AFT CABIN MEGAPHONE BATTERY DEAD. MEGAPHONE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MEGAPHONE PER MM 25-61-14. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,634 hrs · 16,895 cycles
ON FLIGHT 3650 THE CREW REPORTED THE CABIN CEILING EMERGENCY FLOODLIGHT NR 6 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IN NR 6 CABIN CEILING EMERGENCY FLOOD LIGHT IAW CRJ700 AMM 33-51-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 22,746 hrs · 16,362 cycles
DURING MAINTENANCE INSPECTION ON THE FIRST FLIGHT POWER UP, MAINTENANCE NOTICED A STRONG ACRID ODOR THROUGH THE FORWARD CABIN AND COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED ENTIRE AIRCRAFT. NO DAMAGE OR FAULTS NOTED. NO CIRCUIT BREAKER POPPED. POWERED AIRCRAFT AND RAN ALL SYSTEMS. NO ODOR OR FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FIREWALL — DAMAGED (LT PYLON) · airframe 22,676 hrs · 16,314 cycles
DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT PYLON-FIREWALL HAS ELONGATED HOLE AT THE HYDRAULIC FITTING. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR IAW EO CR-54MR-081. THE AIRCRAFT WAS RETURNED TO SERVICE.
2011
Part: FLASHLIGHT — DAMAGED (COCKPIT) · airframe 22,389 hrs · 16,150 cycles
FOR FLIGHT 3607 THE CREW REPORTED THE FIRST OFFICERâS FLASHLIGHT ON/OFF SWITCH WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: HOLDER — BROKEN (COCKPIT) · airframe 22,322 hrs · 16,105 cycles
ON FLIGHT 3850 THE CREW REPORTED THE AFT FLASHLIGHT CAME OUT OF THE BRACKET AT LANDING. THE HOLDER MAY BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT (EMERGENCY) IAW CRJ-700 AMM 25-61-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,143 hrs · 15,317 cycles
DURING MAINTENANCE BASE VISIT WHILE ACCOMPLISHING EMERGENCY LIGHT OPERATIONAL CHECK FOUND FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERABLE ON AFT LEFT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,094 hrs · 14,628 cycles
FOR FLIGHT 4262 THE CREW REPORTED DURING THE PREFLIGHT INSPECTION THE 5 CABIN EMERGENCY EXIT LIGHTS WILL NOT STAY ON FOR MORE THAN 30 SECONDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACKS PER W/C 33-002 OPS CHECKED GOOD. NR 1 P/N 2013-1A, S/N 69968, NR 2 P/N 2013-1A, S/N 104867, NR 3 P/N 2013-1A, S/N 67900, NR 4 P/N 2013-1A, S/N 13239. THE AIRCRAFT WAS RETURNED TO SERVICE.
2010
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,766 hrs · 14,430 cycles
DURING MAINTENACE BASE VISIT FOUND THE LEFT EXTERIOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IAW CRJ 700 AMM 33-51-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,313 hrs · 13,504 cycles
ON FLIGHT 3825 DURING CRUISE THE CREW REPORTED THE CAPTAINâS WINDSHIELD OUTER LAYER SHATTERED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO OMA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW CRJ 700 AMM 56-11-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,868 hrs · 13,199 cycles
ON FLIGHT 2757 THE CREW REPORTED THAT THE PORTABLE MEGAPHONE DOES NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PORTABLE MEGAPHONE ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,275 hrs · 12,794 cycles
ON FLIGHT 4027 THE CREW REPORTED THAT THE EMERGENCY LIGHT SWITCH WAS LEFT IN THE ON POSITION. THE EMERGENCY LIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACKS NR 1 THROUGH NR 4 IAW CRJ 700 AMM 33-51-17. THE OPERATIONAL CHECK WAS GOOD. THE SERIAL NUMBERS: NR 1, 70984, NR 2, 105214, NR 3, 79757 AND NR 4, 73139. THE AIRCRAFT WAS RETURNED TO SERVICE.
2007
Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 11,463 hrs · 8,382 cycles
DURING 2C CHECK INSPECTION REVEALED STA 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICED IN FRAME 280, SUPPORT AND EXTENSION MOUNTS IAW AEA EO CR-53MR AIRCRAFT RETURNED TO SERVICE.
Part: WEB — CORRODED (BS 280) · corrosion level 2 · airframe 11,463 hrs · 8,382 cycles
DURING 3C CHECK INSPECTION REVEALED RIGHT WEB AT STA 280 CORRODED IN SEVERAL LOCATIONS. SPLICED IN NEW WEB AT STA 280 IAW AEA EO CR-53MR-135. AIRCRAFT RETURNED TO SERVICE.
Part: WINDOW — CRACKED (ZONE 200) · airframe 11,434 hrs · 8,359 cycles
CAPTAINS LEFT SIDE WINDOW CRACKED ON SHORT FINAL. REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW CRJ AMM 56-12-01. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE
Part: TORQUE LINK — WORN (RT MLG) · airframe 10,914 hrs · 7,976 cycles
VIBRATION FELT FROM RIGHT MAIN GEAR ON LANDING. REMOVED AND REPLACED RIGHT MAIN GEAR UPPER AND LOWER TORQUE LINKS AND SHIMMY DAMPENER IAW CRJ AMM 23-11-37, 32-11-39 AND 32-11-40. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
2006
Part: SELECTOR VALVE — FAILED (NLG STEERING)
LANDING GEAR DID NOT EXTEND DURING NORMAL EXTENSION. RECEIVED GEAR DISAGREE WARNING WITH LANDING GEAR LEVER DOWN. EXTENDED GEAR USING LANDING GEAR MANUAL RELEASE. NOSE WHEEL STEERING INOPERATIVE. RAI SELECTOR VALVE AND OPS CHECK GOOD. PERFORMED STEERING SYSTEM CHECK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CONTROL UNIT — MALFUNCTIONED (FUEL SYSTEM)
LBB - FLT 3661 - SMOKE COMING FROM REFUEL/DEFUEL PANEL WHEN POWERED ON BY FUELER. REMOVED AND REPLACED REFUEL/DEFUEL CONTROL UNIT IAW CRJ AMM 28-25-18 AND OPS CHECKED IAW CRJ AMM 28-25-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ACM — FAILED (RT ACM)
RT PACK AUTO FAIL, SMOKE AND SMELL COMING FROM CABIN. REPLACED RT ACM, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ACM — SMOKE (RIGHT)
FA REPORTS SMOKE AND ODOR COMING FROM CABIN, MAINTENANCE TROUBLESHOT TO RT PACK ACM CAUSING SMOKE. DEFERRED RIGHT PACK PER MEL 21-13. MAINTENANCE CLEARED MEL BY RAI RIGHT ACM, ACCOMPLISHED POWER RUNS. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)
Part: RELAY — STUCK (EMERGENCY LIGHTS)
EMERGENCY LIGHTS COME ON WITH AIRCRAFT POWEREED BY APU OR ENGINE WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. REPLACED RELAY K135. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)
2003
Part: VALVE — FAILED (MLG)
LANDING GEAR WOULD NOT EXTEND HAD TO EXTEND GEAR MANUALLY. RT LANDING GEAR SELECTOR VALVE. PERFORMED GEAR SWING, AIRCRAFT RETURNED TO SERVICE. (M)