N703SK
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.
246 reports on file, 2004-03-30 – 2026-08-20.
Part: SLAT SYSTEM — FAULTED · airframe 53,921 hrs · 36,962 cycles
IN FLIGHT RECEIVED A SLATS FAIL CAUTION MESSAGE. FAILED AT 1 DEGREE. WHEN WE PUT THE FLAPS TO 45 FOR LANDING, THE SLATS WENT TO 25. (FLIGHT 4325) OPEN
Part: INTERCOSTAL — GOUGED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
AFT EQUIPMENT BAY RT INTERCOSTAL GOUGED AT RT 9 STRINGER APPROX. FS 1144 . REPAIRED AFT EQUIPMENT BAY RT INTERCOSTAL AT RT 9 STRINGER APPROX. BS 1144 IAW REO 670-53-61-2736 DATED 2026-06-16 REV-- ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT WING SLAT TRACK 3-1 IS CHAFED. REPAIRED LT WING SLAT TRACK 3-1 IAW REO 670-57-42-2474 REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT WING SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REPAIR OF LT WING SLAT TRACK 1-3 IAW REO 670-57-42-2473 REV -.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT WING SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REPAIR OF LH WING SLAT TRACK 2-1 IAW REO REO 670-57-42-2485 REV--. COMPLIED WITH 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
FLOORBEAM ANGLE AT BS 280, RBL 11 CORRODED. REPLACED FLOOR BEAM ANGLE/CLIP AT BS 280, RBL 11 WITH NEW. IAW SRM 51-42-06-001-001-A01 & DWG CC670-34191, REV NC, DWG CC67033052 REV -G AND DWG CC670-34010 REV -J. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
Part: STRIKER — CORRODED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SERVICE DOOR LOWER SEAL STRICKER IS CORRODED. REPLACED SERVICE DOOR LOWER SEAL STRIKER IAW DWG SH670-31950, REV Y, & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
GALLEY SERVICE DOOR LOWER SILL IS CORRODED JUST FORWARD OF THE FORWARD DOOR FITTING. REPLACED ANGLE LOWER SILL REF DWG SH670-31950 REV Y & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: TIE BAR — GOUGED (ZONE 400) · airframe 53,685 hrs · 36,594 cycles
LEFT ENGINE FAN COWL, PYLON TIE BAR HAS A GOUGE ON FWD SIDE WHERE IT ATTACHES TO THE PYLON. REPAIRED LT ENGINE FAN COWL, PYLON TIE BAR IAW REO 670-54-12-895, REV -.
Part: TIE BAR — CHAFED (ZONE 400) · airframe 53,685 hrs · 36,594 cycles
LEFT HAND FAN COWL - PYLON TIE BAR, UPPER ATTACHMENT POINT ON PYLON BRACKET CHAFED. REMOVED CHAFE FROM L/H FAN COWL PYLON TIE BAR UPPER ATTACHMENT POINT ON PYLON BRACKET PER IAW SRM 51-12-00-001-001-A01, REWORKED AREA FOUND TO BE WITHIN LIMITS IAW REO 670-54-51-092, REV -.
Part: DOUBLER — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR AFT PULL IN CAM DOUBLER . REMOVED AND INSTALLED NEW PAX DOOR AFT PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N.
Part: DOUBLER — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR FWD PULL IN CAM DOUBLER. REMOVED AND INSTALLED NEW PAX DOOR FWD PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY.
Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR FWD DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801-A01, LEAK TESTED GOOD, NO DEFECTS NOTED.
Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR AFT DD1 INTERCOSTAL MX 32130057. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801-A01, LEAK TEST GOOD NO DEFECTS NOTED. COMPLIED WITH TASK CARD 51-900-1002.
Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR FWD DD1 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801-A01. LEAK TESTED GOOD, NO DEFECTS NOTED.
Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
SUSPECTED CRACK ON PAX DOOR AFT DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801-A01. LEAK TESTED GOOD, NO DEFECTS NOTED.
Part: ANGLE — OUT OF LIMITS (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
REMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME. REPLACED NEW ANGLE AT BS 280 LT IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DWG CC670-33199, REV B, AND DWG CC670-33052, REV-F
Part: SKIN — CRACKED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
UPON REMOVAL OF PAX DOOR INNER SKIN FOUND AFT FORMER CRACKED. INSTALLED NEW AFT FORMER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N.
Part: FLOOR SUPPORT — OUT OF LIMITS (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
REMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME AS CC670-33199(-4 OPP) REMOVED AND REPLACED L/H COCKPIT FLOOR SUPPORT ANGLE (CC670-33199-4) WITH NEW PER REF CRJ 550 SRM 51-42-06-001-001-A01 DWG# CC670-33052, REV -G. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
RIGHT CROSSBEAM AT BS 280 CRACKED ON UPPER FLANGE. REPLACED RT CROSSBEAM AT BS 280 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV K.
Part: WEB — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
RIGHT LOWER WEB AT FS 280 HAS CORROSION. REMOVED AND INSTALLED NEW FABRICATED RT LOWER WEB AT BS 280 IAW SRM 53-11-10-201-003-A01, REV 38 .
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
COCKPIT FLOORBEAM BS 280, LBL 12.00 CRACKED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM IAW SRM 53-11-43-201-003-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
CORROSION ON STRINGER 20L BETWEEN BS 319 AND 333. REMOVED AND REPLACED STRINGER 20L BETWEEN BS 310 AND 349 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH67031810 REV. Y. INSTALLED FASTENERS TO NEW STRINGER 20L BETWEEN BS 319 AND 333 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV. Y.REMOVE FRAME SECTIONS AT FS319.00 AND FS333.00 FOR REMOVAL OF STGR 20L SEE JOB HN00311940 MXTRANS #32209978 FOR REMOVAL AND REPLACEMENT OF STGR20L COMPLIED WITH TASK CARD 51-900-1002
Part: FITTING — CORRODED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
PASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS 314 CORRODED. INSTALLED A NEW FWD CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG.SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY TASK CARD.
Part: CUP — CORRODED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
PASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS342.00 CORRODED. INSTALLED NEW AFT CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY TASK CARD.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
PASSENGER DOOR FLOOR SILL ANGLE BETWEEN BS 310 TO BS 349 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW MID CAP ANGLE TO PAX DOOR LOWER SILL ANGLE REF DWG. SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
COCKPIT FLOORBEAM AT BS 280, RBL 12 CRACKED AND CORRODED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM AT BS 280, RBL 12 IAW SRM 53-11-43-201-003-A01.
Part: FRAME — CRACKED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
CRACK AT BS 333 BETWEEN S1R AND S2R. CRACK AT BS 333 BETWEEN S1R & S2R. REPAIRED BS 333 FRAME BETWEEN STRINGERS 1R - 2R. IAW REO 670-53-21-2863, REV -. ALSO COMPLIED WITH 51-900-1002-SKY.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
DURING AUDIT OF 1C TASK CARD 53-140-509, DETAILED INSPECTION OF THE BS 280 CROSSBEAM, DRAIN PANS AND DRAIN TUBES, FOUND A SUSPECTED CRACKED ANGLE ON THE AFT SIDE OF THE BS 280 CROSSBEAM OTBD OF RBL 9 SHEAR BOX. REMOVED OLD ANGLE & REPLACED WITH 1 EA OF NEW ANGLE ON THE AFT SIDE OF THE BS 280 CROSSBEAM OTBD OF RBL 9 IAW SRM 51-42-21-001-001-A01, REV 38. AND DWG CC670-34010, REV -K.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
RIGHT FLOOR SUPPORT FROM BS 280 - 319.70 WAS CORRODED. REMOVED AND INSTALLED NEW RT FLOOR SUPPORT BS280 - 319.70, STRINGER 17R IAW DWG SH670-32172, REV E, DWG SH670-32170, REV V, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-13-001-001-A01. NO LEAKS NOTED.
Part: MOUNT — CORRODED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
FORWARD CARGO BAY, FWD CARGO NET MOUNTING PLATE CORRODDED APROX FS 533 BETWEEN S23-24 LT. REPLACED AND INSTALLED NEW BRACKET SH670-33389-1, IAW DWG.SH670-33600 REV AD, SRM.51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. ALSO COMPLIED WITH 51-900-1002-SKY AND SEE CONTINUATION CARD FOR DETAILS
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
PAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS. INSTALLED NEW PAX DOOR LOWER SILL ANGLE REF BOMBARDIER DWG SH670-31810 REV AE, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY TASK CARD.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
LEFT SIDE FLOOR SUPPORT BS 280 - 310 CORRODED. REMOVED AND INSTALLED NEW LT FLOOR SILL FROM BS 280 TO 310 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-40-11-001-001-A01, SRM 51-42-13-001-001-A01, AND DWG SH670-32170, REV V.
Part: ROLLER GUIDE — DENTED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
AFT CARGO DOOR UPPER GUIDE ROLLER TRACKS DENTED IN MULTIPLE SPOTS. COMPLIED WITH SRM 53-61-58-201-002-A01 TRACK REPAIR, INSTALLED NEW LOWER TRACK SECTION REF REO 670-53-61-1296, REV --.
Part: MOUNT — CORRODED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 CENTER STRG 27. REMOVED AND REPLACED WITH NEW FWD CARGO BAY AFT CARGO NET MOUNTING PLATE. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. IAW DWG SH670-33600 REV AD, SRM 51-40-11-001-001-A01.
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
AFT CARGO DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS AROUND SCREW HOLES. REPLACED AFT CARGO LOWER SILL. IAW DWG MM670-35085 REV K, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, & SRM 51-42-21-001-001-A01.
Part: MOUNT BRACKET — CORRODED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 BETWEEN STRG 23-24. REPLACED FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE APROX BS 581 BETWEEN S23-24. IAW DWG SH670-33600, REV AD, & SRM 51-42-21-001-001-A01.
Part: SLAT TRACK — GOUGED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT SLAT TRACK 3-2 HAS GOUGES ON INBOARD EDGE AND LOWER SURFACES. REPAIRED LEFT SLAT TRACK 3-2 PER REO 670-57-42-2475, REV --, STEPS 1-7. OPS AND RIG CHECKED GOOD.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 53,685 hrs · 36,594 cycles
RIGHT SLAT TRACK 3-3 CHAFED ON LOWER SIDE. REPAIRED RH SLAT TRACK 3-3 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2478 REV-.
Part: SLAT TRACK — GOUGED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT SLAT TRACK 2-2 HAS GOUGES ON INBOARD EDGE AND LOWER SURFACE. REPAIRED LT SLAT TRACK 2-2 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2477 REV--.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 53,685 hrs · 36,594 cycles
RIGHT SLAT TRACK 2-2 CHAFED ON LOWER AND INBD SIDE. REPAIRED RT SLAT TRACK 2-2 LOWER INBD SIDE IAW SRM 51-12-00-001-001-A01, REO 670-57-42-2479, REV --.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 53,685 hrs · 36,594 cycles
RIGHT SLAT TRACK 1-3 CHAFED ON LOWER SIDE REWORKED THE RT SLAT TRACK 1-3 IAW REO 670-57-42-2480, REV-.
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 53,685 hrs · 36,594 cycles
RIGHT SLAT TRACK 2-1 CHAFED ON LOWER SIDE. BLENDED SLAT TRACK REWORKED RH SLAT TRACK 2-1 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2472 REV --, ALL STEPS COMPLIED WITH.
Part: SLAT TRACK — CHAFED (ZONE 500) · airframe 53,685 hrs · 36,594 cycles
LEFT SLAT TRACK 3-3 CHAFED ON LOWER SURFACE. REPAIRED LT SLAT TRACK 3-3 PER REO 670-57-42-2476, REV-,
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 53,685 hrs · 36,594 cycles
RIGHT SLAT TRACK 1-2 CHAFED ON LOWER SIDE. REWORKED RT SLAT TRACK 1-2 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2481 REV--.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 53,685 hrs · 36,594 cycles
RIGHT UPPER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED THE CRACKED STANDOFF AND INSTALLED A NEW STANDOFF ON R/H UPPER TRANSCOWL, IAW GREO #670-54-21-971, REV -B, STEP 1-3.
Part: PLATE — CRACKED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
FORWARD EQUIPMENT COMPARTMENT RIGHT SIDE ADG PUMP REINFORCEMENT PLATE CRACKED. PERFORMED REPAIR TO FORWARD EQUIPMENT COMPARTMENT RIGHT SIDE ADG PUMP REINFORCEMENT PLATE & INSTALLED NEW DOUBLER IAW SRM 53-11-43-201-001-A01. REVISION 38,
Part: LUG — DAMAGED (ZONE 800) · airframe 53,685 hrs · 36,594 cycles
PASSENGER DOORS DOOR SIDE OF THE HINGE LUG 27 ROLL PIN HOLE IS ELONGATED. DRILLED AND LOCATED NEW PAX DOOR PIANO HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01, STEPS E, F, G, H, I AND SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG 601R31702, REV N. INSTALLED NEW PAX DOOR PIANO HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01, STEPS R, S, T, U, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG 601R31702 REV N,.PRESSURIZED AIRCRAFT IAW AMM 21-31-00-910-801-A01. LEAK TESTED GOOD, NO DEFECTS NOTED.
Part: SKIN — SCRATCHED (ZONE 200) · airframe 53,685 hrs · 36,594 cycles
MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO BS 1051.30 BETWEEN S27R AND S24R. REPAIRED MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO 1051.30 BETWEEN S27R AND S24R. IAW REO 670-53-61-2715 REV -.
Part: RECEPTACLE — CRACKED (TRU) · airframe 53,685 hrs · 36,594 cycles
RIGHT TRU LANDING AFT LATCH RECEPTACLE CRACKED. INSTALLED NEW RIGHT TRU LANDING IAW REO 670-53-11-2304 REV-.
Part: RECEPTACLE — CRACKED (TRU) · airframe 53,685 hrs · 36,594 cycles
LEFT TRU LANDING AFT LATCH RECEPTACLE CRACKED. REPAIRED LT TRU LANDING AFT LATCH RECEPTACLE. PER REO 670-53-11-2304 REV -A, SRM 51-42-06-001-001-A01, AND DWG CC670-33040 REV G.
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 53,685 hrs · 36,594 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA96506-REO 670-53-00-077 MXCODEID107216-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 96506COMPLIED WITH REO 670-53-00-077 REV: D DATED: 2018-07-23 ALTERNATE FASTENER FOR TEMPORARY POTABLE WATER DRAIN MAST INSTALLATION FOR RH MIDDLE NUTPLATE ON AFT DRAIN MASTTHIS TEMPORARY DISPOSITION IS VALID FOR 8000 FLIGHT HOURS FROM THE TIME OF ITS INCOPORATION, REPLACED DRAIN MAST CHANNEL DAMAGE, AND INSTALLED NEW CHANNEL ON BS 1031 TO BS 1051.30, S27 REF DWG MM670-43200 REV N . AND SRM 51-42-06-001-001-A01. PRESSURE CHECKS GOOD.
Earlier reports · 2004–2025 · 194 reports
2025
Part: WINDSHIELD — ARCED (ZONE 200) · airframe 52,251 hrs · 35,122 cycles
LEFT WINDSHIELD ARCING DURING FLIGHT. LH WSHLD SWITCH TURNED OFF. ARCING STOPPED. MEL 30-41-1ACAT C DUE 5/24/25LEFT WINDSHIELD ARCING DURING FLIGHT. LH WSHLD SWITCH TURNED OFF. ARCING STOPPED. (FILED CLOSED) REMOVED AND REPLACED LH WINDSHIELD IN REF WITH TASK CARD 56-220-1000-SKY. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.
2021
Part: ROLLER — DEFORMED (LT SLAT TRACK) · airframe 45,713 hrs · 29,429 cycles
LH SLAT TRACK 1-2 4EA SIDE ROLLERS WORN OUT OF LIMITS. (C-CHECK RO 8/31/21) REMOVED AND RE-INSTALLED 4EA NEW SERVICEABLE ROLLERS ON LH SLAT TRACK 1-2 IAW CRJ 700 AMM 27-81-44-000/400-801-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: ROLLER — DEFORMED (RT SLAT TRACK) · airframe 45,713 hrs · 29,429 cycles
RH SLAT TRACK 1-2 HAS 4EA SIDE ROLLERS WITH FLAT SPOTS OUT OF LIMITS, AND REQUIRE REPLACEMENT. (C-CHECK RO 8/31/21) REMOVED AND REPLACED RH 1-2 4EA SIDE ROLLERS IAW CRJ 700 AMM 27-81-44-000/400-801-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED
Part: STRAP — DAMAGED (BS 202) · airframe 45,713 hrs · 29,429 cycles
DISCREPANCY TRANSFERED FROM CAMP CARD 22928499: JOB# 910139123 OP: 2 REMOVE AND REPLACE LOWER LH STRAP AT F.S 202.75 REF: DWG: CC670-34125 PER STEP1 OF REPAIR INSTRUCTION OF MHIRJ REO 670-53-11-1704 REV: -- DATE: 2021-06-17 (C-CHECK RO 8/31/21) REPAIRED LOWER LH STRAP AT FS202.75 IAW MHI REO 670-53-11-1704 REV. --, DATED 06-17-2021. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FRAME — CORRODED (BS 379 S19R) · airframe 45,713 hrs · 29,429 cycles
FRAME CORRODED AT FS 379 STRINGER 19R (C-CHECK RO 8/31/21) CORRODED FRAME SECTION FROM FS 379 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 REV. 38 B DATED 12/14/2020. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: STRINGER — CORRODED (BS 280-295 S27) · airframe 45,713 hrs · 29,429 cycles
FOUND CORROSION DAMAGE @ STRINGER 27 BETWEEN F.S.280-F.S.295 (C-CHECK RO 8/31/21) REMOVED AND REPLACED WITH NEW STRINGER 27 SECTION FROM F.S 280 TO FS. 295 IAW CRJ 700 SRM 51-42-06-001-001-A01. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FLOOR SUPPORT — NOT REPORTED · airframe 45,713 hrs · 29,429 cycles
REPLACE R/H FLOOR SILL FROM FS 1031.00 TO FS 1051.30 FROM JOB# 910139124 OP# 32 CAMP # 22623336. (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H FLOOR SILL (SIDE BEAM PN# MM670-35404-001 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 45,713 hrs · 29,429 cycles
REPLACE R/H FLOOR SILL FROM FS 1015.00 TO FS 1031.00 FROM JOB# 910139124 OP# 32 CAMP # 22623336. (C-CHECK RO 8/31/21) REPLACED R/H FLOOR SILL FROM FS 1015.00 TO FS 1031.00 IAW CRJ 700 SRM 51-42-06-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE ATTAHCED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: STRINGER — CORRODED (BS 310-319 S19R) · airframe 45,713 hrs · 29,429 cycles
FOUND CORROSION AT STRINGER 19R BETWEEN FS310 AND FS319 (C-CHECK RO 8/31/21) REMOVED AND REPLACED STRINGER 19R IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-021-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 295-310 S20R) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL BETWEEN FS295 AND FS310 STRINGER 20R FOUND CORRODED. SH670-32047-951. (C-CHECK RO 8/31/21) INTERCOSTAL BETWEEN FS295 AND FS310 STRINGER 20R SH670-32047-951 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: STRINGER — CORRODED (BS 349 S22R) · airframe 45,713 hrs · 29,429 cycles
STRINGER 22R FOUND CORRODED JUST FWD OF FS349 (C-CHECK RO 8/31/21) REMOVED AND REPLACED STRINGER 22R JUST FWD OF FS349 IAW CRJ700 SRM 51-42-06-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 333-349 S21L) · airframe 45,713 hrs · 29,429 cycles
BACKUP SILL INTERCOSTAL AT STGR 21L F.S. 333-349 FOUND TO BE CORRODED (C-CHECK RO 8/31/21) BACKUP SILL INTERCOSTAL AT STGR 21L F.S. 333-349 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-004-A01 & 51-42-21-001-001-A01. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHT CHANGE
Part: FRAME — CORRODED (BS 320) · airframe 45,713 hrs · 29,429 cycles
FRAME AT FS320.00 IS CORRODED. (C-CHECK RO 8/31/21) FRAME AT FS 320.00 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: FORMER — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PASSENGER DOOR FORMER AT F.S.320.163 IS CORRODED ALONG ITS ENTIRE LENGTH. (C-CHECK RO 8/31/21) PAX DOOR FORMER @ FS 320.163 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: FRAME — CORRODED (BS 327.76) · airframe 45,713 hrs · 29,429 cycles
FRAME AT FS 327.76 FROM DD6 TO DD8 IS CORRODED. (C-CHECK RO 8/31/21) FRAME @ FS 327.76 FROM DD6 TO DD8 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: CLEAT — CORRODED (BS 312) · airframe 45,713 hrs · 29,429 cycles
CLEAT AT INTERSECTION OF DD4 AND 312.56 IS CORRODED. (C-CHECK RO 8/31/21) CLEAT @ INTERSECTION OF DD4 & 312.56 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: SUPPORT ANGLE — CORRODED (BS 311) · airframe 45,713 hrs · 29,429 cycles
FORWARD SUPPORT ANGLE AT FS311.76 IS CORRODED. (C-CHECK RO 8/31/21) FWD SUPPORT ANGLE @ FS 311.76 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 311-320) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD3 FROM FS311 TO FS320 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD3 FROM FS 311 TO FS 320 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 312-320) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD7 BETWEEN FS312.56 AND FS320.16 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD7 BETWEEN FS 312.56 AND 320.16 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 338-347) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD3 BETWEEN FS338.9 AND FS347.2 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD3 BETWEEN FS 338.9 AND 347.2 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 312-320) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD5 BETWEEN FS312.56 AND FS320.16 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD5 BETWEEN FS 312.56 AND FS 320.16 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A0 REV 38B DATED 14 DEC 2020. INTERCOSTAL WAS RECEIVED AND REQUIRED MODIFICATION IN ORDER TO INSTALL. PART WAS MODIFIED IAW REO 670-52-11-1239 REV. -- DATED 2021-02-04. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 312-320) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD2 BETWEEN FS312.56 AND FS320.16 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD2 BETWEEN FS312.56 AND 320.16 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 311-320) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD4 BETWEEN FS311.76 AND FS320.16 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD4 BETWEEN FS 311.76 AND 320 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 338-347) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD5 BETWEEN FS338.9 AND FS347.2 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD5 BETWEEN FS 338.9 & 347.2 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 323-335) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD1 BETWEEN FS323 AND FS335 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD1 BETWEEN FS323 AND 335 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: BRACKET — CORRODED (BS 311.76) · airframe 45,713 hrs · 29,429 cycles
BRACKET AT INTERSECTION OF DD5 AND 311.76 FORMER IS CORRODED. (C-CHECK RO 8/31/21) BRACKET @ INSTECTION OF DD5 AND 311.76 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FORMER — CORRODED (BS 313.56) · airframe 45,713 hrs · 29,429 cycles
FORMER AT FS313.56 IS SEVERELY CORRODED ALONG ITS ENTIRE LENGTH. (C-CHECK RO 8/31/21) FORMER AT FS 313.56 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 338-347) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD2 FROM FS338 TO FS347 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD2 FROM FS338 TO 347 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (BS 323-335) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD1A FROM FS323 TO FS335 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD1A FROM FS323 TO 335 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 338-347) · airframe 45,713 hrs · 29,429 cycles
INTERCOSTAL AT DD4 BETWEEN FS338 AND FS347 IS CORRODED. (C-CHECK RO 8/31/21) INTERCOSTAL AT DD4 BETWEEN FS 338 & FS 347 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: DOUBLER — CRACKED (DOOR) · airframe 45,713 hrs · 29,429 cycles
AFT PULL-IN CAM DOUBLER IS CRACKED AND CORRODED. (C-CHECK RO 8/31/21) AFT PULL IN CAM DOUBLER WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FRAME — CORRODED (BS 313.59) · airframe 45,713 hrs · 29,429 cycles
FRAME AT FS313.59 BETWEEN DD4 AND DD5 IS CORRODED. (C-CHECK RO 8/31/21) FRAME AT FS313.59 BETWEEN DD4 AND DD5 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: BRACKET — CORRODED (BS 311.76) · airframe 45,713 hrs · 29,429 cycles
BRACKET AT INTERSECTION OF DD3 AND 311.76 FORMER IS CORRODED. (C-CHECK RO 8/31/21) BRACKET @ INTERSECTION OF DD3 AND 311.76 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: HINGE — GOUGED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR HINGE GOUGED ON AFT DOOR SILL SIDE APPROX. .040" (C-CHECK RO 8/31/21) REMOVED AN REPLACED PAX DOOR HINGE WITH NEW SERVICEABLE HINGE IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 53-21-23-201-007-A01 REV. 38B,DATED 12/14/2020. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM 337 COMPLETED AND ATTACHED. WEIGHT CHANGE NEGILIBLE.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR INTERCOSTAL DD06 CORRODED AT FS 320.163 TO FS 338.963. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD6 BETWEEN FS 320.16 AND 338.963 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR INTERCOSTAL AT DD03 CORRODED FROM FS 320.163 TO FS338.963. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD3 BETWEEN FS 320.163 AND 338.963 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR INTERCOSTAL AT DD02 CORRODED AT FS 320.163 TO FS 338.963. (C-CHECK RO 8/31/21) INTERCOSTAL @ DD2 BETWEEN FS 320.16 AND 338.963 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR INTERCOSTAL DD07 CORRODED AT FS 320.167 TO 338.963 (C-CHECK RO 8/31/21) INTERCOSTAL @ DD7 BETWEEN FS 320.167 AND 338.963 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: SKIN — CHAFED (BS 969-985 S27) · airframe 45,713 hrs · 29,429 cycles
EXTERNAL SKIN CHAFED BETWEEN FS969.00 AND FS985.00 AT STRGR 27 (C-CHECK RO 8/31/21) REPAIRED EXTERNAL SKIN IAW MHI REO 670-53-00-661 REV.--, DATED 6/2/21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 45,713 hrs · 29,429 cycles
PAX DOOR INTERCOSTAL AT DD04 CORRODED FROM FS 320.163 TO FS 338.963 (C-CHECK RO 8/31/21) INTERCOSTAL @ DD4 BETWEEN FS 320.163 AND 338.963 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NO DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: SKIN — CORRODED (LT WING TE) · airframe 45,713 hrs · 29,429 cycles
L/H WING TRAILING EDGE UPPER SKIN AT OUTBOARD MULTI FUNCTION SPOILER SKIN HAS SEVERAL WORKING FASTENERS. (C-CHECK RO 8/31/21) REMOVED AND REPLACED 4 WORKING RIVETS ON L/H WING T/E UPPER SKIN AT OTBD MULTI FUNCTION SPOILER SKIN IAW CRJ 700 SRM 51-42-06-001-001-A01.
Part: ATTACH BOLT — CORRODED (LT SPOILER PCU) · airframe 45,713 hrs · 29,429 cycles
L/H WING OUTBOARD GROUND SPOILER PCU ATTACH BOLT AND NUT CORRODED. (C-CHECK RO 8/31/21) NEW NUT AND BOLT INSTALLED IAW CRJ 700 AMM 27-63-01-400-801-A01 REFERENCE REMAINING STEPS IN CAMP# 22247325
Part: SLAT TRACK — GROOVED (RT WING) · airframe 45,713 hrs · 29,429 cycles
R/H WING # 1 SLAT TRACK 1-1 IS GROOVED ON LOWER EDGE. (C-CHECK RO 8/31/21) REMOVED AND REPLACED THE RH WING #1 SLAT TRACK 1-1 IAW CRJ 700 AMM 27-81-41-000/400-801-A01. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED
Part: ATTACH BOLT — CORRODED (LT WING TE FLAP) · airframe 45,713 hrs · 29,429 cycles
L/H OUTBOARD FLAP, OUTBOARD FLAP HINGE LUG LOWER FITTING ATTACH BOLT NUT IS CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED LH OUTBOARD FLAP, OUTBOARD HINGE LUG LOWER FITTING ATTACH NUT AND WASHER IAW CRJ700 AMM 57-53-27-400-803-A01.
Part: SLAT TRACK — GROOVED (RT WING) · airframe 45,713 hrs · 29,429 cycles
R/H WING #3 SLAT TRACK 3-3 IS GROOVED ON LOWER EDGE. (C-CHECK RO 8/31/21) REMOVED AND REPLACED THE RH WING #3 SLAT TRACK 3-3 IAW CRJ 700 AMM 27-81-41-000/400-803-A01. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED
Part: FRAME — CORRODED (BS 319 S25-26L) · airframe 45,713 hrs · 29,429 cycles
FS 319 FRAME IS CORRODED FROM STRINGER 25L TO 25R. (C-CHECK RO 8/31/21) REMOVED AND REPLACED FRAME SECTOR IAW CRJ700 SRM 53-00-06-201-006-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 45,713 hrs · 29,429 cycles
L/H INTERCOSTAL FROM FS 349 TO FS 364 IS CORRODED (C-CHECK RO 8/31/21) REMOVED AND INSTALLED L/H INTERCOSTAL FROM FS 349 TO FS 364 IAW CRJ-700 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-25-16-001-001-A01 AND 51-40-11-001-001-A01 REV 38B-14DEC2020, FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED, NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
Part: FLOORBEAM — CORRODED (BS 1051 LBL27-36) · airframe 45,713 hrs · 29,429 cycles
CROSSBEAM AT FS1051.20 HAS MULTIPLE SPOTS OF CORROSION BETWEEN LBL27 AND LBL36 (C-CHECK RO 8/31/21) REPAIRED CROSSBEAM AT FS1051.20 BETWEEN LBL27 AND LBL36 IAW REO 670-53-61-1879 REV -- DATED 2021-04-30 FPRM 337 AND MAJOR REAPIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFROMED
Part: SEAT TRACK — CORRODED (BS 517-585 LBL9) · airframe 45,713 hrs · 29,429 cycles
FLOOR SEAT TRACK AT LBL 9 FS517.00 TO FS 585.00 CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE L/H FLOOR SEAT TRACK AT LBL 9 FROM FS 517.00 TO FS 585.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — CORRODED (BS 577-677) · airframe 45,713 hrs · 29,429 cycles
R/H SIDE SEAT TRACK STR R 15 DA 577.00 TO FS 677.00 PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED R/H SIDE SEAT RAIL FROM STR R 15 AT FS 577.00 TO FS 677.00 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL FROM FS 577.00 TO FS 677.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — GOUGED (BS 437) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT RAIL STR 15 FS 437.00 GOUGED. (C-CHECK RO 8/31/21) REMOVED GOUGED L/H SIDE SEAT RAIL STR L 15 AT FS437.00 IAW CRJ-700 AMM 53-00-49-000-801-A03 AND INSTALLED SERVICABLE L/H SIDE SEAT RAIL STR L 15 AT FS437.00 IAW CRJ-700 AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 678-761) · airframe 45,713 hrs · 29,429 cycles
R/H SIDE SEAT TRACK FS 678.00 TO FS 761.85 AT STR 15R PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H SEAT TRACK AT STR15 F.S. 678 TO F.S. 761 IAW CRJ700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03
Part: SEAT TRACK — CORRODED (BS 485-581 RBL9) · airframe 45,713 hrs · 29,429 cycles
R/H FLOOR SEAT TRACK RBL 9 FS 485.00 TO FS 581.00 IS PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED SEAT TRACK AT RBL 9 FS 485.00 TO FS 581.00 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL 9 FS 485.00 TO FS 581.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: ANGLE — CORRODED (BS 280 L-RBL 9) · airframe 45,713 hrs · 29,429 cycles
FWD "J" ANGLE IS CORRODED AT FS 280 BETWEEN LBL 9 AND RBL 9 (C-CHECK RO 8/31/21) FWD "J" ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-06-001-001-A01. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 985-1000) · airframe 45,713 hrs · 29,429 cycles
LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS985.00 TO FS1000.00 (C-CHECK RO 8/31/21) REMOVED AND REPLACED SILL IAW REO 670-53-61-1900 REV -- DATED 2021-05-20, REFER TO CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 864-969) · airframe 45,713 hrs · 29,429 cycles
R/H SIDE SEAT TRACK STR R15 FS 864.00 TO FS 969.00 PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H SIDE SEAT STR R15 F.S. 864 TO 969 IAW CRJ700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03
Part: FLOORBEAM — CORRODED (BS 280) · airframe 45,713 hrs · 29,429 cycles
AVIONICS FLOORBOARD SUPPORT AT FS 280 IS CORRODED (C-CHECK RO 8/31/21) AVIONICS FLOORBOARD SUPPORT AT FS 280 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — GOUGED (BS 581-677) · airframe 45,713 hrs · 29,429 cycles
FLOOR SEAT TRACK AT RBL 9 FS 581.00 TO FS677.00 PITTED, GOUGED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED R/H FLOOR SEAT TRACK AT RBL 9 FROM FS 581.00 TO FS 677.00 IAW CRJ700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK AT RBL 9 FROM FS 581.00 TO FS 677.00 IAW CRJ700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — CORRODED (BS 527-575) · airframe 45,713 hrs · 29,429 cycles
R/H SIDE SEAT TRACK STR 15 FS 527.00 TO FS 575.00 IS PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED OLD AND INSTALLED NEW SERVIABLE SEAT TRACK ON RH SIDE LOCATED AT TR 15 FS 527.00 TO FS 575.00 IAW CRJ700 AMM 53-00-49-400-801(A03). REFERENCE CAMP# 22868878 FOR FAB OF NEWE PART. REF CONTIUATION CARD FOR DETAILS OF WORK PERFROMED
Part: SEAT TRACK — CORRODED (BS 709-761) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT TRACK AT STR L 15 FS 709.00 TO FS 761.00 CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED TWO LH SIDE SEAT TRACKS AT STR L 15 FROM FS 645.00 TO FS 714.00 AND FROM FS 714.00 TO FS761.00 IAW CRJ 700 AMM TASK 53-00-49-000-801 (CONFIG A03) AND CRJ 700 AMMTASK 53-00-49-400-801 (CONFIG A03)
Part: SEAT TRACK — CORRODED (BS 349-394 LBL9) · airframe 45,713 hrs · 29,429 cycles
R/H FLOOR SEAT TRACK AT LBL 9 FS 349.00 TO FS 394.00 IS PITTED AND CORRODED (C-CHECK RO 8/31/21) FOUND DISCREPANCY TO BE @ RH FLOOR SEAT TRACK AT RBL 9 FS349-485. RH SEAT TRACK AT RBL 9 FS349-485 WAS REMOVED AND REPLACED IAW CRJ 700 AMM 53-00-49-000-801-A03. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 864-923) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT TRACK AT STR L 15 FS 864.00 TO FS 923.00 PITTED AND CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED L/H SIDE SEAT RAIL AT FS 864.00 TO FS 923.00 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE L/H SIDE SEAT RAIL AT FS 864.00 TO FS 923.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT TRACK AT STR L15 AND FS 785.15 TO FS 863.00 CORRODED AND GOUGED. (C-CHECK RO 8/31/21) REMOVED CORRODED L/H SIDE SEAT TRACK FROM FS 785.15 TO FS 863.00 IAW CRJ700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE L/H SIDE SEAT TRACK FROM FS 785.15 TO FS 863.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — CORRODED (BS 668-708) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT RAIL STR L 15 AT FS 668.00 TO FS 708.00 CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED LH SIDE SEAT RAIL STR L 15 AT FS 668.00 TO FS 708.00 IAW CRJ 700 AMM TASK 53-00-49-000-801 (CONFIG A03) AND CRJ 700 AMM TASK 53-00-49-400-801 (CONFIG A03)
Part: SEAT TRACK — CORRODED (BS 586-667) · airframe 45,713 hrs · 29,429 cycles
FLOOR SEAT RAIL AT LBL9 FS 586.00 TO FS 667.00 CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED SEAT TRACK AT LBL 9 FROM FS 586.00 TO FS 667.00 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL 9 FROM FS 586.00 TO FS 667.00 IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: SEAT TRACK — CORRODED (BS 586-677) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT RAIL AT STR L15 FS 586.00 TO FS 677.OO CORRODED AND PITTED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED WITH NEW L/H SIDE SEAT RAIL AT STR15L F.S. 586.00 TO F.S. 677.00 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03
Part: FRAME — CORRODED (BS 310 S25L-R) · airframe 45,713 hrs · 29,429 cycles
FS 310 FRAME IS CORRODED FROM STRINGER 25L TO 25R. (C-CHECK RO 8/31/21) REPAIRED FS 310 FRAME FROM STRINGER 25L TO 25R IAW CRJ-700 SRM 53-00-06-201-006-A01, 51-25-16-001-001-A01, 51-42-21-001-001-A01 REV 38B DATED 14 DEC 2020. TASK CARD 51-900-1002-SKY IS COMPLETE, FORM M-337 IS ATTACHED. NO CHANGE TO WEIGHT AND BALANCE. OP AND LEAK CHECKS GOOD. REFERENCE CONTINUATION FOR WORK PERFORMED. / PRESSURE CHECKS DUE
Part: FLOOR SUPPORT — CORRODED (BS 985-1088 LBL9) · airframe 45,713 hrs · 29,429 cycles
FLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM FS985.00 TO FS1088.20 (C-CHECK RO 8/31/21) FLOOR BEAM AT LBL9 FROM FS985.00 TO FS1088.20 WAS REPAIRED IAW CRJ700 SRM 53-00-41-201-001-A01.COMPLETED AND ATTACHED FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY. ADDED WEIGHT FOR FLOOR BEAM REPAIR 1.72LB, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 45,713 hrs · 29,429 cycles
R/H SIDE SEAT TRACK STR R 15 FS 785.15 TO FS 863.00 CORRODED AND PITTED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H SEAT RAIL AT STR 15R F.S. 785 TO 863 IAW CRJ700 SRM 51-41-02-001-001-A01 AND AMM 53-00-49-400-801-A03
Part: SEAT TRACK — GOUGED (BS 465) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT RAIL STR L 15 AT FS 465.00 HAS GOUGE IN TRACK. (C-CHECK RO 8/31/21) REMOVED AND REPLACED L/H SIDE SEAT RAIL STR L 15 AT FS 483.00 TO FS 379.00 IAW CRJ 700 AMM TASK 53-00-49-000-801 (CONFIG A03) AND CRJ 700 AMMTASK 53-00-49-400-801 (CONFIG A03)
Part: STRINGER — CORRODED (BS 310-349 S20R) · airframe 45,713 hrs · 29,429 cycles
STRINGER 20R FROM FS 310 TO FS 349 IS CORRODED (C-CHECK RO 8/31/21) STRINGER 20R FROM FS 310 TO FS 349 IS CORROSION WAS FOUND TO BE ON INTERCOSTALS, INTERCOSTALS WERE REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 45,713 hrs · 29,429 cycles
AFT CARGO DOOR SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION FROM FS1000.00 TO FS1047.00 (C-CHECK RO 8/31/21) REMOVED CORRODED AFT CARGO DOOR SILL ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED SERVICABLE AFT CARGO DOOR SILL ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A0 . OP CHECKS GOOD. REFERENCE CONTINUATION FOR WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 985-1088) · airframe 45,713 hrs · 29,429 cycles
RH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS985.00 TO FS1088.20 (C-CHECK RO 8/31/21) REMOVED AND REPLACED RH FLOOR SILL (SIDE BEAM) FROM FS985.00 TO FS1088.20 IAW MHI REO 670-53-61-1913 REV. --, DATED 6/1/21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 45,713 hrs · 29,429 cycles
SEAT TRACK AT LBL 9 FROM FS 379.0 TO FS 477.0 IS CORRODED. (C-CHECK RO 8/31/21) REMOVED CORRODED SEAT TRACK AT LBL 9 FROM FS 379.00 TO FS 477.00 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND FABRICATED NEW SERVICEABLE L/H FLOOR SEAT TRACK IAW CRJ700 SRM 53-00-39-201-002-A01 AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03
Part: FITTING — CORRODED (BS 265-280) · airframe 45,713 hrs · 29,429 cycles
FORWARD JACK FITTING INTERCOSTALS R/H AND L/H ARE CORRODED FROM FS 265 TO FS 280. (C-CHECK RO 8/31/21) INSTALLED JACK FITTING AND NEW INTERCOSTALS PN: CC670-32179-1 AND CC670-32179-2 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01 REV 38B-14DEC2020 REF: BOMBARDIER DWG: CC670-32050 REV:NC FOR FASTENER CALL OUT, RESTORED FINISH AS REQUIRED IAW CRJ 700 SRM51-25-16-001-001-A01 REV 38B-14DEC2020.M-337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 1000-1088) · airframe 45,713 hrs · 29,429 cycles
FLOOR BEAM AT LBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000.00 TO FS1088.20 (C-CHECK RO 8/31/21) REMOVED AND REPLACED FLOOR BEAM FROM FS 977 TO FS1057 AND OUTBOARD SPLICE ANGLES IAW CRJ-700 SRM 53-00-41-201-001-A01. M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: STRINGER — CORRODED (BS 310-349 S20L) · airframe 45,713 hrs · 29,429 cycles
STRINGER 20L FROM FS 310.0 TO FS 349.0 IS CORRODED (C-CHECK RO 8/31/21) REMOVED AND REPLACED STRINGER 20L IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-021-001-001-A01. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. OP CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 485-585) · airframe 45,713 hrs · 29,429 cycles
L/H SIDE SEAT RAIL STR L 15 R AT FS485.00 TO FS 585.00 IS CORRODED AND PITTED. (C-CHECK RO 8/31/21) REMOVED CORRODED L/H SIDE SEAT RAIL STR L 15 R AT FS485.00 TO FS 585.00 IAW CRJ-700 AMM 53-00-49-000-801-A03 AND INSTALLED SERVICABLE L/H SIDE SEAT RAIL STR L 15 R AT FS485.00 TO FS 585.00 IAW CRJ-700 AMM 53-00-49-400-801-A03.
Part: FRAME — CORRODED (BS 319 S18-19L) · airframe 45,713 hrs · 29,429 cycles
FS 319.0 IS CORRODED FROM STRINGER 18L TO 19L ON FRONT AND BACK SIDES. (C-CHECK RO 8/31/21) FS 319.0 IS CORRODED FROM STRINGER 18L TO 19L WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. & DRAWING SH670-31810 REVY. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 45,713 hrs · 29,429 cycles
R/H WING O/B FLAP UPPER SURFACE PANELS HAVE CORRODED HARDWARE (C-CHECK RO 8/31/21) REPLACED CORRODED HARDWARE ON R/H O/B FLAP AND INSTALLED ALL NEW HARDWARE IAW CRJ 700 SRM 51-21-00-001-001-A01
Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 45,713 hrs · 29,429 cycles
L/H WING O/B FLAP UPPER EXTERNAL SKIN HAS NUMEROUS SMOKING RIVETS. (C-CHECK RO 8/31/2021)REMOVED AND REPAIRED 56 SMOKING RIVETS ON L/H WING O/B FLAP UPPER EXTERNAL SKIN AS REQUIRED IAW REO 670-57-53-275 REV A DATED 2021-05-20. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED, NO WEIGHT CHANGE. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — DAMAGED (RT WING UPPER) · airframe 45,713 hrs · 29,429 cycles
R/H WING O/B FLAP TOP SKIN HAS NUMEROUS SMOKING RIVETS (C-CHECK RO 8/31/21) REMOVED OLD SMOKING RIVETS AND INSTALLED NEW SERVICABLE ONES ON R/H WING O/B FLAP TOP SKIN IAW REO 670-57-53-274 REV-A DATED 2021-05-20. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED, SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — DENTED (ZONE 100) · airframe 45,713 hrs · 29,429 cycles
SMALL DENT ON FWD FUSELAGE BELLY FWD AND OB OF TCAS ANTENNA. IF WITHIN ACCEPTABLE LIMITS REMOVE ALL EVIDENCE USING STANDARD ACFT PRACTICES (C-CHECK RO 8/31/21) SMALL DENT ON FWD FUSELAGE BELLY FWD AND OB OF TCAS ANTENNA WAS REPAIRED IAW CRJ 700 SRM 53-00-01-201-001-A01. NO FURTHER DEFECTS NOTED. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED, WEIGHT 1.06LBS ADDED. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — CRACKED (ZONE 100) · airframe 45,713 hrs · 29,429 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA66797-670-53-11-1659 703SK MXCODEID54914-PR - SUSPECT CRACK FOUND ON THE SKIN BELOW THE LT TRU DOOR LOWER AFT CORNER. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1659 REV-- DATE 2021-02-23. PERMANENT REPAIR WITHIN 300 FLIGHT HOURS DUE BY TAT 45769.2, PART NUMBER: - , SERIAL NUMBER: 10139, POSITION: ( C-CHECK RO 8/31/2021) COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA66797-670-53-11-1659 703SK MXCODEID54914-PR - SUSPECT CRACK FOUND ON THE SKIN BELOW THE LT TRU DOOR LOWER AFT CORNER. COMPLIED WITH PERMANENT REPAIR IAW REO 670-53-11-1706-REV-- DATED 2021-06-27. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — DENTED (GROUND SPOILER) · airframe 45,713 hrs · 29,429 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA62136-670-57-71-065 703S MXCODEID52984-PR - RT WING INBD GROUND SPOILER HAS MULTIPLE SHALLOW DENTS. COMPLIED WITH TEMPORARY REPAIR PER REO 670-57-71-065. PERMANENT REPAIR DUE WITHIN 1000 FLT HRS DUE AT OR BEFORE TAT 45749.50, PART NUMBER: - , SERIAL NUMBER: 10139, POSITION: (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H INBD GROUND SPOILER IAW CRJ 700 AMM 27-65-01-400-801-A01 RIG AND OPS GOOD
Part: SKIN — DENTED (BS 235 S26L-R) · airframe 45,713 hrs · 29,429 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA42074-670-53-11-1382-PR - FOUND 3 DENTS LOCATED ON FS235.00, BETWEEN STGR-26L AND STGR-26R. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1382. PERMANENT REPAIR DUE WITHIN 6500 FLT HRS PER REO 670-53-11-1382 REV A DATED 2019-08-16 DUE BY TAT: 46009.7., PART NUMBER: - , SERIAL NUMBER: 10139, POSITION: 3 DENTS LOCATED ON FS235.00, BETWEEN STGR-26L AND STGR-26R WERE REPAIRED IAW MHIRJ REO 670-53-11-1687 REV-- DATED 2021-06-15 AND CRJ 700 SRM 51-42-06-001-A01 REV. 38B 12/14/2020. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED.NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — DENTED (GROUND SPOILER) · airframe 45,713 hrs · 29,429 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA62135-670-57-72-040 703SK MXCODEID52982-PR - RT WING OUTBD GROUND SPOILER HAS MULTIPLE SHALLOW DENTS. COMPLIED WITH TEMPORARY REPAIR PER REO 670-57-72-040. PERMANENT REPAIR DUE WITHIN 1000 FLT HRS DUE AT OR BEFORE TAT 45749.50, PART NUMBER: - , SERIAL NUMBER: 10139, POSITION: (C-CHECK RO 8/31/21) REMOVED AND REPLACED R/H OUTBD GROUND SPOILER IAW CRJ 700 AMM 27-65-05-400-801-A01 RIG AND OPS GOOD
Part: SKIN — DENTED (GROUND SPOILER) · airframe 45,713 hrs · 29,429 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA62133-670-57-72-039 703SK MXCODEID52978-PR - LT WING OUTBD GROUND SPOILER HAS MULTIPLE SHALLOW DENTS. COMPLIED WITH TEMPORARY REPAIR PER REO 670-57-72-039. PERMANENT REPAIR DUE WITHIN 1000 FLT HRS DUE AT OR BEFORE TAT 45749.50, PART NUMBER: - , SERIAL NUMBER: 10139, POSITION: (C-CHECK RO 8/31/21) REMOVED AND REPLACED L/H OUTBD GRPOND SPOILER IAW CRJ 700 AMM 27-65-05-400-801-A01
2018
Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 40,132 hrs · 24,872 cycles
RUDDER TRIM WENT FULL NOSE LEFT ONCE WE GOT TO CRUISE. (FLT 2975) FO: 7/16/18 CLOSED / REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. OPS CHECK GOOD AT THIS TIME.
2017
Part: POST — CRACKED (BS 202 BULKHEAD) · airframe 38,506 hrs · 23,538 cycles
ONE CRACK INDICATION NOTED ON THE RBL 30 POST, ON FWD SIDE OF THE BS 202 BULKHEAD. .200 INCH LONG. REPAIRED THE POST IAW SRM.
Part: POST — CRACKED (BS 202 BULKHEAD) · airframe 38,506 hrs · 23,538 cycles
ONE CRACK INDICATION NOTED ON LBL 30 POST ON THE FWD SIDE OF THE BS 202 BULKHEAD. .350 INCH LONG. REPAIRED THE POST IAW SRM.
Part: FRAME — CRACKED (BS 235) · airframe 38,506 hrs · 23,538 cycles
BS 235 FRAME HAS A VISUALLY INSPECTED CRACK ADJACENT TO THE UPPER MOST LIGHTNING HOLE. REMOVED AND THE FRAME IAW SRM.
Part: FRAME — CRACKED (BS 220) · airframe 38,506 hrs · 23,538 cycles
RIGHT BS 220 FRAME HAS A CRACK INDICATION NOTED AT FASTENER HOLE ADJACENT TO LIGHTNING HOLE JUST BELOW STRINGER 13AR, .150 INCH LONG. REMOVED AND REPLACED THE FRAME IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 37,742 hrs · 22,999 cycles
BS 280 TO 319.7 RIGHT FLOOR SUPPORT HAS MULTIPLE CORROSION AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. ALL CHECKED GOOD.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,742 hrs · 22,999 cycles
BS 280 FLOORBEAM ANGLE CORRODED. INSTALLED A NEW FLOORBEAM ANGLE IAW SRM.
2015
Part: SKIN — DENTED (BS 202) · airframe 34,051 hrs · 20,179 cycles
FOUND DENT ON SKIN PANEL, AT FS 202.75 BETWEEN LBL 22.0 AND LBL 30.0 DUE TO BIRDSTRIKE DAMAGE. DAMAGE IS OUT OF LIMITS IAW SRM. REMOVED SKIN PANEL, PN CC670-33105-1, JUST AFT OF LT TRU DOOR AND INSTALLED A NEW SKIN PANEL IAW SRM AND REO.
Part: HINGE — GOUGED (PAX DOOR) · airframe 33,333 hrs · 19,733 cycles
PASSENGER DOOR HINGE-FUSELAGE SIDE-GOUGED AT AFTMOST LANDING, FROM HINGE PIN RETENTION PIN. C-CHECK RO 5/23/15, BLENDED OUT GOUGED ON PAX DOOR HINGE FUSELADGE SIDE, BLENDED SECTION OF HINGE MEASURED AT 0.500" L, 0.600" W, 0.055" D, BLENDED SECTION OF HINGE FOUND WITH IN LIMIT REF STS EA. R & R HINGE PIN AND SPRING PIN TO CORRECT THE CAUSE OF CHAFE REF AMM.
Part: DOOR FRAME — CRACKED · airframe 33,333 hrs · 19,733 cycles
PAX DOOR AFT FRAME FORMER IS CRACKED AT RETRACT CABLE PULLEY MOUNT ATTACH POINTS. REMOVED AFT FRAME FORMER FROM DOOR REF SRM. INSTALLED NEW AFT FORMER TO PAX DOOR IAW SRM.
Part: SKIN — GOUGED (LT NACELLE) · airframe 33,333 hrs · 19,733 cycles
INTERIOR OF LT LOWER FWD CORE COWL GOUGED. JUST AFT OF ENGINE DRAIN HOLES. C-CHECK RO 5/23/15, COMPLIED WITH REPAIR OF LT LOWER FWD CORE COWL FIRE-SHIELD GOUGE. IAW REO.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,333 hrs · 19,733 cycles
PASSENGER DOOR INTERCOSTAL CORRODED, ABOVE PRESSURE DOOR CUT OUT. REMOVED CORROSION, NDT'D, EVALUATED, FOUND TO BE WITHIN LIMITS, RESTORED FINISH IAW STS EA.
Part: STEP — CORRODED (PAX DOOR) · airframe 33,333 hrs · 19,733 cycles
PAX DOOR BOTTOM STEP PANEL ASSY HAS CORROSION AT BOTTOM FLANGE. REPAIRED PAX DOOR BOTTOM STEP PANEL ASSY AT BOTTOM FLANGE REF EA.
Part: SKIN — DENTED (BS 1000-1015) · airframe 33,117 hrs · 19,600 cycles
TWO DENTS JUST BELOW THE AFT BAGGAGE BAY DOOR BS 1000 -1015 BETWEEN STRINGERS 15 AND 16L. REPAIRED IAW REO.
Part: SKIN — CORRODED (E/E BAY DOOR) · airframe 33,333 hrs · 19,733 cycles
CORROSION PRESENT AT INSIDE LIP SKIN OF MAIN AVIONICS BAY DOOR OPENING. REMOVED CORROSION IAW REO. REINSPECT IAW REO REQUIREMENTS AND IAW NDTM. C-CHECK RO 5/23/15. REMOVED CORROSION IAW REO.
2014
Part: RECEIVER — FAULTY (LOCALIZER) · airframe 32,163 hrs · 19,057 cycles
LOCALIZER RECEIVERS FAIL INTERMITTENTLY. R & R NR 1 AND 2 VIR-432 IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,210 hrs · 18,546 cycles
FWD LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R FWD LEFT NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM. OPS CHECKED GOOD.
Part: TRU — FAILED (NR 2) · airframe 30,444 hrs · 18,127 cycles
NR 2 TRU IS SMOKING. R & R THE TRU ,
Part: SEAL — DIRTY (PAX DOOR) · airframe 30,412 hrs · 18,109 cycles
MAIN CABIN DOOR HANDLE STICKS AND WILL NOT OPEN. CLEANED MAIN CABIN DOOR SEAL AS REQUIRED. DOOR OPERATES NORMALLY. NO DEFECTS NOTED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,928 hrs · 17,859 cycles
EMERGENCY EXIT SIGN IS BURNED OUT, REPLACED LAMP.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 29,821 hrs · 17,792 cycles
RECEIVED CABIN ALT WARNING MESSAGE. FOLLOWED QRH PROCEDURE. SMELL OF SMOKE & LIGHT HAZE IN THE CABIN. FLT 5506 REPLACED NR 1 ACSC IAW AMM. OPERATIONS CHECKED GOOD. PRESSURIZED AIRCRAFT WITH NO FAULTS IN MANUAL MODE. NO HAZE OR SMOKE SMELL DETECTED DURING PRESSURIZATION. SUSPECT HAZE & SMOKE SMELL CAME FROM 02 GENERATORS, PN ON OFF GG690-95028-5, SN ON 00913 & SN OFF 00887A.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,714 hrs · 17,733 cycles
CTR CEILING EMERGENCY LIGHT BETWEEN ROWS 20 & 21 IS BURNED OUT. FLT 5176 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,527 hrs · 17,630 cycles
EMERGENCY EXIT FLOOD LIGHTS AT MAIN CABIN DOOR BULB IS BURNED OUT. FLT 5189 RELAMPED.
2013
Part: LUG — CORRODED (HORIZ STAB) · airframe 29,104 hrs · 17,398 cycles
HORIZONTAL STABILIZER LUG NR 1 OTBD FACE HAS FRETTING, 1ST LUG FROM THE LEFT. C-CHECK REPAIRED DAMAGE ON HORIZONTAL STABILIZER LUG NR 1 OTBD FACE, 1ST LUG FROM THE LEFT IAW REO.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
RT FS 280 LOWER BULKHEAD WEB IS CORRODED BEYOND LIMITS. C-CHECK REPLACED RT FS 280 LOWER BULKHEAD WEB IAW REO.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
LT FS 280 LOWER BULKHEAD WEB IS CORRODED BEYOND LIMITS. C-CHECK REPLACED LT FS 280 LOWER BULKHEAD WEB IAW REO.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
LT COCKPIT FLOOR BEAM CRACKED AT FS 274 LBL 12 WL 71.5. C-CHECK REPAIRED LT CRACKED FLOOR BEAM AT FS 274, LBL 12, WL 71.5, IAW REO.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
RT COCKPIT FLOOR BEAM CRACKED AT FS 274 RBL 12 WL 71.5. C-CHECK REPAIRED RT CRACKED FLOOR BEAM AT FS 274, RBL 12, WL 71.5 IAW REO.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
CRACK AT INTERNAL FWD EQUIPMENT COMPARTMENT CLOSE TO TRUÃâ¬â¢S WL79.50 & FS202.75. C-CHECK REPAIRED CRACK AT INTERNAL FWD EQUIPMENT COMPARTMENT CLOSE TO TRUÃâ¬â¢S WL79.50 & FS202.75 IAW REO.
Part: DOOR — CHAFED (PAX DOOR) · airframe 29,104 hrs · 17,398 cycles
PAX DOOR FWD PULL-IN LEVER ASSEMBLY CHAFED. C-CHECK REPAIRED PAX DOOR PULL-IN LEVER ASSEMBLY IAW REO.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 29,104 hrs · 17,398 cycles
CRACK AT FWD EQUIPMENT COMPARTMENT CLOSE TO ADG PUMP WL79.50 & FS202.75. C-CHECK REPAIRED CRACK AT FWD EQUIPMENT COMPARTMENT CLOSE TO ADG PUMP WL79.50 & FS202.75 IAW REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,975 hrs · 16,754 cycles
EMERGENCY OVERHEAD LIGHT IN GALLEY REAR IS BURNED OUT. FLT#6213 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,816 hrs · 16,663 cycles
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. RELAMPED.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,227 hrs · 15,729 cycles
NR 2 OVERHEAD LIGHT IN CABIN BURNED OUT. (FLT 6476) RELAMPED OVERHEAD LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,088 hrs · 15,649 cycles
AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5601) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,068 hrs · 15,638 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5526) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,502 hrs · 15,300 cycles
LEFT EMERGENCY ROW OVERHEAD LIGHT STRIP IS INOPERATIVE. (FLT 5177) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,558 hrs · 14,755 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5497) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,286 hrs · 14,607 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,174 hrs · 14,551 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5326) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,116 hrs · 14,517 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6483) RELAMPED EMERGENCY LIGHT.
Part: MCU — FAILED (STABILIZER) · airframe 24,094 hrs · 14,507 cycles
STAB CHANNEL 1 IS INOPERATIVE. (FLT 5204) REPLACED THE MCU IN REF TO AMM. P/N 7074-5 S/N OFF 435.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,926 hrs · 14,417 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6421) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,523 hrs · 14,216 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,523 hrs · 14,216 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6259) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,514 hrs · 14,212 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,325 hrs · 14,103 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6230) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,214 hrs · 14,051 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6425) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,155 hrs · 14,011 cycles
OVERHEAD AFT EMERGENCY LIGHT IS OUT. (FLT 5507) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,974 hrs · 13,918 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5156) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,974 hrs · 13,918 cycles
RIGHT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5160) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,891 hrs · 13,878 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5529) RELAMPED EMERGENCY LIGHT.
Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 22,891 hrs · 13,878 cycles
SMELL OF SMOKE IN COCKPIT. (FLT 5459) TRACED SMELL OF SMOKE TO FMS CDU. REPLACED FMS CDU. P/N 822-0021-202 S N OFF 34C9N
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,701 hrs · 13,778 cycles
NR 5 OVERHEAD EMERGENCY LIGHT DOES NOT WORK. (FLT 6462) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,331 hrs · 13,564 cycles
NR 3 AND NR 5 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6351) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,322 hrs · 13,558 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6209) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,274 hrs · 13,528 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6237) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,274 hrs · 13,528 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6231)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,227 hrs · 13,500 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6203) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,102 hrs · 13,417 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6389) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,962 hrs · 13,331 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 5322) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,717 hrs · 13,208 cycles
THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT. (FLT 6289) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,629 hrs · 13,162 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,526 hrs · 13,110 cycles
AFT MOST OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,526 hrs · 13,110 cycles
OVERHEAD EMERGENCY LIGHT BURNED OUT BY ROW 10. (FLT 1197) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,114 hrs · 12,880 cycles
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 7007) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,068 hrs · 12,859 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,022 hrs · 12,835 cycles
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 1150) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,557 hrs · 12,559 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6503) RELAMPED EMERGENCY LIGHT.
2010
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,610 hrs · 12,005 cycles
FS 280 FLOORBEAM CORRODED OUT OF LIMITS. (C-CHECK) REPLACE FS 280 FLOORBEAM PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,875 hrs · 12,154 cycles
FOUND CORROSION OUT OF LIMITS ON FS 280 FLOORBEAM. (C-CHECK) REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,608 hrs · 10,815 cycles
CEILING EMERGENCY LIGHT AT ROW 10 INOP. (FLT 5827) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,443 hrs · 10,720 cycles
EMERGENCY OVERHEAD FLOODLIGHT NR 3 INOP. (FLT 6089) RELAMPED EMERGENCY LIGHT.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,779 hrs · 10,316 cycles
THE MOST AFT CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. (FLT 6278)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,687 hrs · 9,645 cycles
EMERGENCY LIGHT AT ROW 15 INOP. (FLT 6053) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,452 hrs · 9,519 cycles
AFT EMERGENCY CEILING LIGHT INOP. (FLT 6572) RELAMPED EMERGENCY LIGHT.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 15,140 hrs · 9,347 cycles
FLT 6452 - OXYGEN LEAK IN COCKPIT OVERHEAD PANEL. REPLACED OBSERVER MASK AND CREW OXYGEN BOTTLE.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,120 hrs · 9,337 cycles
FLT 6448 - SECOND TO LAST CEILING EMERGENCY LIGHT INOP. RELAMPED.
Part: SKIN — CHAFED (RT AILERON) · airframe 15,511 hrs · 9,556 cycles
RIGHT AILERON LEADING EDGE SKIN CHAFED. (C CHECK) REPLACED PER SRM.
Part: SELECTOR VALVE — FAILED (MLG) · airframe 14,107 hrs · 8,759 cycles
FLT 6467 - "GEAR DISAGREE" WARNING ILLUMINATED. GEAR EXTENDED WITH MANUAL RELEASE. REPLACED MLG SELECTOR VALVE, PN: 53340-7.
2008
Part: STRUT — DISCHARGED (NLG) · airframe 12,914 hrs · 8,030 cycles
"STEERING INOP" CAUTION MSG. AFTER TAKEOFF, NLG STRUT BOTTOMED OUT. OPS CHECK OF NLG STEERING NORMAL.
Part: WINDOW — CRACKED (COCKPIT) · airframe 11,980 hrs · 7,485 cycles
FLT 6716 - COPILOT SIDE WINDOW IS CRACKED. REPLACED COPILOT'S SIDE WINDOW IAW MM 56-11-01. ALL OPS CHECKS GOOD, P/N OFF 601R33033-18, S/N OFF 03321H8789.
Part: STRIP — DAMAGED (CABIN) · airframe 11,506 hrs · 7,204 cycles
FLT 5911 - FORWARD EMERGENCY LIGHT STRIP IS DAMAGED. REPLACED LIGHT STRIP IAW 33-31-01.
Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 10,991 hrs · 6,907 cycles
FLT 5876 - RECEIVED A "SMOKE AFT LAV" WARNING MESSAGE. INSPECTED LAV AREA AND ASSOCIATED SYSTEMS WITH NO DEFECTS NOTED.
2007
Part: FIXTURE — BROKEN (EMERGENCY LIGHTS) · airframe 10,666 hrs · 6,709 cycles
FLT 6048 - EMERGENCY LIGHT ON THE GALLEY WALL IS BROKEN. REPLACED FLOOR LEVEL FLOOD LIGHT FIXTURE IN GALLEY IAW CRJ AMM 33-51-11.
Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 10,001 hrs · 6,295 cycles
FLT 6570 - EMERGENCY EXIT SIGN IS MISSING AT ROW 3. FOUND EMERGENCY EXIT SIGN COVER AND REINSTALLED IT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,310 hrs · 5,878 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 16 IS OUT. RELAMPED OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD.
Part: WIRE — SHORTED (CHART LIGHT) · airframe 8,221 hrs · 5,214 cycles
FO'S CHART HOLDER LIGHT SPARKED, THEN WENT OUT. REPAIRED CHART LIGHT POWER SUPPLY IAW WDM 20-33-00 AND ALSO REPLACED LAMP CONTROL ASSEMBLY. OPERATIONAL CHECKS GOOD.
2006
Part: UNKNOWN — ODOR (CABIN) · airframe 7,539 hrs · 4,766 cycles
SMOKE LAV WARNING MESSAGE AFTER TAKEOFF WITH SMELL OF SMOKE THROUGHOUT CABIN. RETURNED TO TUS. RAN PACKS WITH BOTH APU AND ENGINE BLEED AIR PER MM 71-00-00, 21-00-00 AND THE SMOKE ODOR DISSIPATED. UNABLE TO DUPLICATE DISCREPANCY.
Part: WEB — CRACKED (PAX DOOR) · airframe 7,764 hrs · 4,916 cycles
PAX DOOR FWD WEB AT 2ND STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT 2ND STEP FWD SIDE OF PAX DOOR PER REO 670-52-11-104 REV B.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,764 hrs · 4,916 cycles
PAX DOOR OUTER HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED OUTER HANDLE PER CRJ7/9 AMM 51-11-03-400-801-A01. OPERATIONAL CHECKS GOOD.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 7,764 hrs · 4,916 cycles
COCKPIT FLOORBOARD AT SUPPORT ATTACHED 280 BEAM IS CRACKED AT THE LT AND RT SIDES, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FLOOR SUPPORT AFT COCKPIT PART NR CC670-33282-13 P/O 74023 PER SRM 51-42-21.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,764 hrs · 4,916 cycles
280 BEAM CRACKED AT LOWER AND UPPER SIDES BRACKETS ON THE LT AND RT SIDES, DISCOVERED DURING C-CHECK INSPECTION. INSTALL NEW CROSSBEAM AT FR ST 280 PER 1S70531100026 AND SRM 51-42-06-001-001-A01.
Part: WEB — CRACKED (PAX DOOR) · airframe 7,764 hrs · 4,916 cycles
PAX DOOR AFT WEB AT 2ND STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PART AT AFT WEB 2ND STEP PER REO 670-52-11-104 REV B.
Part: WEB — CRACKED (PAX DOOR) · airframe 7,764 hrs · 4,916 cycles
PAX DOOR AFT WEB AT 3RD STOP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT 3RD STEP AFT SIDE OF PAX DOOR PER REO 67052-11-104 REV 'B'.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,764 hrs · 4,916 cycles
PAX DOOR AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED AFT PAX DOOR DRAG ANGLE PER REO 670-52-11-072.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 4,795 hrs · 2,984 cycles
RECEIVED SSCU 2 STATUS AND PITCH FEEL MSG'S. REPLACED SSCU2 IAW MM 27-61-05. OPERATIONAL CHECK GOOD.
2005
Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 4,465 hrs · 2,762 cycles
"SLATS FAIL" MSG ON POWER-UP. REPLACED RT SENSOR, BRAKE POSITION UNIT IAW CRJ 700 MM 27-52-03. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 4,380 hrs · 2,702 cycles
SPOILER/STAB FAILED. REPLACED NR 2 SSCU IAW CRJ MM ATA CHAPT 27-61-05. OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 3,626 hrs · 2,231 cycles
EMERGENCY LIGHTS SWITCH ON F/A PANEL LEFT IN "ON" POSITION, EMERGENCY LIGHTS INOP. REPLACED FOUR ELBP'S IAW CRJ 700 MM 33-51-17. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 3,250 hrs · 2,003 cycles
STAB CHANNEL/2 STATUS MESSAGE ON EICAS. REPLACED STAB TRIM MOTOR CONTROL UNIT IAW CRJ 700 MM 27-42-07. OPERATIONAL CHECK GOOD IAW CRJ MM 27-61-05.
Part: DOOR — BINDING (MAIN PAX) · airframe 2,747 hrs · 1,683 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE. LUBED CABIN DOOR. OPERATIONAL CHECK GOOD.
2004
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 2,117 hrs · 1,251 cycles
OUTBOARD SPOILERONS & OUTBOARD GROUND SPOILERS CAUTION MESSAGE. REMOVED AND REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD.
Part: CONTROLLER — MALFUNCTIONED (SLAT/FLAP) · airframe 1,892 hrs · 1,138 cycles
SPLR/STAB FAULT, RUD LIMITER FAULT & PITCH FEEL FAULT DISPLAYED ON EICAS. REMOVED AND REPLACED SFECU NR 1 IAW CRJ MM 27-51-05. COMPLIED WITH SLAT/FLAP AUTO RIG AS REQUIRED. OPERATIONAL CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 1,317 hrs · 836 cycles
RIGHT OVERWING EXIT LOWER EMERGENCY LIGHT INOP. RELAMPED LOWER EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD.
Part: FLAP — OUT OF RIG · airframe 60 hrs · 44 cycles
FLAPS HALF SPEED MSG ON EICAS. RIGGED FLAPS IAW MM 27-52-00-802-A01, TR 27-0190.