N751EV
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Atlantic Southeast Airlines, Inc. | Operator | on 2011-10-23 | Operator named in NTSB report |
Accident & incident history
Operated by ATLANTIC SOUTHEAST AIRLINES INC (per NTSB report)
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.
281 reports on file, 2004-11-08 – 2026-06-15.
Part: TRU — FAULTED · airframe 43,207 hrs · 32,075 cycles
DC BUSS 2 CAUTION MESSAGE. SMELLED A BURNING ODOR FOR ABOUT A MINUTE BEFORE GOING AWAY. MULTIPLE ASSOCIATED FAILURES INCLUDING CAUTION MESSAGES AS WELL AS MANY STATUS MESSAGES. MEL 24-31-1CAT B. SMOD APPROVEL REQUIRED FOR RTS DUE TO ODI EVENT (FLIGHT 4684) UPON ARRIVAL , POWERED ACFT UP & TROUBLESHOT DC BUSS 2 CAUTION PER FIM 24-31-00. ALL MESSAGES CLEARED EXCEPT FOR THE TRU 2 FAIL STATUS REMAINED ILLUMINATED THEREFORE DEFERRED TRU 2 IAW MEL 24-31-1. MX ACTIONS COMPLIED WITH , PLACARDS PLACED . INSPECTED AVIONICS BAY FOR ANY SIGN OF DAMAGE , FOUND NO DAMAGE PRESENT.
Part: CONTROL UNIT — FAULTED (STEERING) · airframe 42,826 hrs · 31,722 cycles
STEERING INOPERATIVE CAUTION AFTER PUSHBACK. RAN QRH MESSAGE CLEARED. (FLIGHT 4710) INTERROGATED MDC AND FOUND FAULT CODE B-007456 FOR NWS ECU FAILED DUE TO INTERNAL FAULT. REMOVED AND REPLACED NWS STEERING ECU REFERENCING APPLICABLE STEPS OF AMM 32-51-10. RIG CHECKS GOOD. PERFORMED MULTIPLE OP CHECKS OF NWS DURING GROUND TAXI RUNS WITH NO ISSUES NOTED, COULD NOT REPEAT STEERING INOP CAUTION MESSAGE.
Earlier reports · 2004–2025 · 279 reports
2025
Part: PLATE — GOUGED · airframe 40,930 hrs · 30,007 cycles
UPON REMOVAL OF CARGO NET MOUNTING PLATE INTERCOSTAL FOUND DEEP GOUGES IN RADIUS. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INTERCOSTAL WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-06-001--001-A01,51-42-21-001-001-A01, 51-45-00-001--001-A01, DWG-SH670-33579 REV-D. NO LEAKS DETECTED.FOR DETAILS SEE CONTINUATION CARD. COMPLIEDWITH TASK CARD 51-900-1002-SKY
Part: FRAME — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FOUND CORROSION ON FWD WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS 295 STR24L ( MX# 29494459 JOB OP: HN00214212 ) (C-CHECK RO 3/14/2025) REPAIRED FWD. WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS295 STR24L IAW REO 670-53-21-2554 REV -- DATED: 2025-02-12. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
CORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE, RH SIDE AT APPROXIMATELY FS 1088. SEE ATTACHED PIC. (C-CHECK RO 3/14/2025) REMOVED CORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE (SILL) REF-CRJ-700 SRM 51-21-06-001-001 A01 AND FOUND AREA RE-WORKED TO BE WITHIN LIMITS REF-CRJ-700 SRM 53-61-43-101-001 A01, SRM 53-00-45-201-001 A01, REMOVED AND INSTALLED NEW AFT BAGGAGE-BAY FLOOR SCREEN SUPPORT ANGLE BRACKET AT RH APPROX FS1088 REF-CRJ-700 SRM 51-42-21-001-001 A01 AND DWG MM670-35041 REV Y. AND COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: LANDING — CRACKED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
RH SIDE TRU BAY DOOR LOWER LANDING HAS A CRACK ON AFT LATCH CUT OUT (C-CHECK RO 3/14/2025) REMOVED AND REPLACED TRU LOWER LANDING WITH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, 51-42-22-001-001-A01 , REO- 670-53-11-2086 REV -- DATE 2025-01-16. (ALTERNATE FASTENERS) COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.
Part: BAYONET — CRACKED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
LEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS ARE CRACKED. 29442703 (C-CHECK RO 3/14/2025) REPAIRED LEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS REF GREO PL 670-52-21-103 REV:--:DATE:2024-11-06
Part: BAYONET — CRACKED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
RIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET IS CRACKED. 29442720 (C-CHECK RO 3/14/2025) REPAIRED RIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET BY COMPLYING WITH ALL STEPS OF REO# 670-52-21-106 REV:-- DATE: 2025-02-03. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
Part: BRACKET — CRACKED (ZONE 500) · airframe 40,930 hrs · 30,007 cycles
S/N 0440LH WING, SLAT TRAK CANISTER BRACKET 1-3 IS CRACKED. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED THE LH WING SLAT TRACK CANNISTER BRACKET AT SLAT TRACK 1-3 REF REO 670-57-42-577 REV -- 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD
2024
Part: PITOT TUBE — SCRATCHED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
R/H PITOT STATIC PROBE CUTOUT ON THE UPPER SKIN AT FS210.00 BETWEEN STGR 14 AND STGR 15 LOWER AFT HOLE HAS MULTIPLE SCRATCHES AS MARKED (C-CHECK RO 3/14/2025) WET INSTALLED NEW REPLACEMENT R/H PITOT STATIC MOUNTING PLATE AT FUSELAGE SKIN FS.210 BETWEEN STGR14R & STGR15R PER CRJ700 SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01. NO LEAKS DETECTED. FOR DETAILS SEE CONTINUATION CARD. COMPLIED WITH TASK CARD 51-900-1002-SKY. CRJ700 SRM TASK 51-42-06-001-001-A01 , SRM TASK 51-42-21-001-001-001-A01, & BOMBARDIER DWG. CC670-33015 REV. -G
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 40,930 hrs · 30,007 cycles
LH AFT VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 40,930 hrs · 30,007 cycles
RH FWD VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED RH FWD VERTICAL STAB DRAG ANGLE IAW MHI RJ R.E.O. 670-55-31-187 REV. -- DATED 2025-02-18 AND COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: PANEL — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
THE RH MLG WHEEL WELL PANEL 642AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 642AZ IN RH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
Part: PANEL — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
THE LH MLG WHEEL WELL PANEL 542AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 542AZ IN LH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REVE. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
Part: COWLING — CHAFED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
S/N 0368LH ENGINE INTERNAL. LOWER CORE COWL HAS MULTIPLE CHAFES AND GOUGES. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED LH ENGINE INTERNAL, LOWER CORE COWL AT MULTIPLE CHAFES AND GOUGES. SEE CONTINUATION CARD FOR FURTHER DETAILS. ALL STEPS OF REO 670-54-23-1284 REV-B, DATED 2025-02-28 COMPLIED WITH. ALL TASKS OF TASK CARD 51-900-1002-SKY COMPLETED
Part: DECK PLATE — DENTED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
S/N 0329UNDER PILOTS SEAT, FLOORING HAS A DENT . FLAGGED (C-CHECK RO 3/14/2025) REPAIRED DENT UNDER PILOTS SEAT, FLOORING REF REO 670-53-11-2081 REV -- DATED 2025-01-23, COMPLIED WITH 51-900-1002-SKY
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
FS280 CLIP ON THE OB SIDE OF LBL12 APPEARS TO BE CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CLIP P/N CC670-34099-1 AT FS280 ON THE OUTBOARD SIDE OF LBL12. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# KBA670-30026 REV. J.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: MOUNT — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 533 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01,51-42-06-001-001-A01,51-45-00-001-001 A01 AND DWG-SH670-33600 REV-AD. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS
Part: MOUNT — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 581 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED FWD BAG BAY CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01, 51-45-00-001-001-A01, 51-42-06-001-001-A01 AND DWG-SH670-33600 REV-AD..COMPLIED WITH 51-900-1002-SKY. SEE OCNTINUE CARD FOR DETAILS
Part: STRAP — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY, FWD H STRAP CORRODED @ APROX FS 538 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP AT F.S.538.00.REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01.DWG-SH670-33750 REV-Y. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).
Part: HINGE — GOUGED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY DOOR HINGE ON ACFT SIDE GOUGED AND WORN. REMOVED AND REPLACED DOOR HINGE FITTING WITH NEW ONE. REF: CRJ-700 S.R.M.51-41-04-001-001-A01,SRM 51-40-11-001-001 A01, DWG-SH670-33840 REV-C TUC--5659 CAL DUE 31-MAR-2025.COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).
Part: STRAP — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY , AFT H STRAP CORRODED @ APROX FS 581 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP WITH NEW ONE AT F.S.581 .REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01 DWG-SH670-33793 REV-A.COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).
Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
CROOS BEAM CAP CORRODED AT APROX FS 1051 RBL 40 MARKED (C-CHECK RO 3/14/2025) CORROSION ON CROSSBEAM CAP FS1051 AT APPROX RBL40 FOUND TO BE OUT OF LIMITS, REPAIRED WITH REO 670-53-61-2449 REV -- DATED 2025-01-22, COMPLIED WITH 51-900-1002-SKY
Part: MOUNT — CORRODED (ZONE 100) · airframe 40,930 hrs · 30,007 cycles
FWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 557 BETWEEN LBL STRG 27-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WIRTH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, DWG-SH670-33574 REV-A. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY
Part: HOUSING — GOUGED (ZONE 800) · airframe 40,930 hrs · 30,007 cycles
AFT CARGO DOOR HANDLE HOUSING IS GOUGED (MARKED) (C-CHECK RO 3/14/2025) REMOVED DAMAGED AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670-38702 REV. F. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28. COMPLIED WITH SKY CARD 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL I/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
Part: RIVET — LOOSE (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
L/H UPPER TRANSCOWL Z STIFFENER RIVETS PULLED LOOSE (C-CHECK RO 3/14/2025) REPAIRED L/H UPPER TRANSCOWL AT LOOSE / PULLED RIVETS ON INNER SKIN COMMON TO ZED STIFFENER, REF. REO 670-54-21-1709, REV. --, 2025-01-24. COMPLIED WITH 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL O/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
Part: SKIN — DENTED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H UPPER TRANSCOWL INNER PERFORATED SKIN IS DENTED (C-CHECK RO 3/14/2025) REPAIRED R/H UPPER TRANSCOWL INNER PERFORATED SKIN AT DENTED LOCATION, REF. CRJ700 SRM 54-10-00-201-002-A01, REPAIR SRS704 AND REO 670-54-21-1703, REV. --, 2025-01-14. COMPLIED WITH 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
Part: COAMING — CHAFED (ZONE 400) · airframe 40,930 hrs · 30,007 cycles
R/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 3/14/2025) REPAIRED INNER LATCH DOOR COAMING AT FWD. LATCH ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-1028, REV. NC, 2009-06-15 AND REO 670-54-21-1705, REV. --, 2025-01-17. AND OPS TEST AND FUNCTIONAL AND RIG CHECK GOOD SEE CONTINUE CARD FOR DETAILS
Part: HINGE — GOUGED (ZONE 200) · airframe 40,930 hrs · 30,007 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA59692-670-53-21-582 N751EV MXCODEID52126-DTI - PAX DOOR HINGE FUSELAGE SIDE HAS NEW GOUGE ON AFT LUG LANDING. REMOVED GOUGE FROM PAX DOOR HINGE (FUSE SIDE) AFT LUG LANDING, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS REF REO 670-53-21-582 REV -F DATED 2017-08-02 TYPE 4. DETAILED VISUAL INSPECT ALL LUGS PER NDTM PART 1, CHAP. 51-20-009 FOR CRACK IN LUG OR LUG FAILURE., PART NUMBER: - , SERIAL NUMBER: 10163, POSITION: (C-CHECK RO 3/14/2025) PERFORMED DETAILED VISUAL INSPECT ALL LUGS PAX DOOR HINGE FUSELAGE SIDE PER NDTM PART 1, CHAP. 51-20-009, FOUND WEAR MARK ON VERY AFT LANDING. COMPLIED WITH REPAIR TO VERY AFT LANDING OF PAX DOOR HINGE FUSELAGE SIDE REF REO 670-53-21-582 REV -G 2024-02-18 TYPE IV. COMPLIED WITH TASK CARD 51-900-1002-SKY. REINSPECT REQUIRED AT 5700 FLIGHT CYCLES
2022
Part: NONE — ODOR · airframe 40,490 hrs · 29,638 cycles
CREW GETTING SMELLS OF BURNING RUBBER. MOSTLY NEAR ROWS 10 AND 16. SEEMS TO BE MORE PROMINENT DURING TAXI. AND EVEN STRONGER DURING BLEED TRANSFERS FROM BOTH ENGINES TO APU AND APU TO ENGINES. (FLIGHT #4959 FILED CLOSED) COMPLIED WITH ADJUSTMENT AND TEST OF AIR CONDITIONING SYSTEM IN REF. TO AMM 21-51-00, WITH NO NOTICEABLE CHANGE IN CABIN AIR QUALITY. THE SYSTEM WAS TESTED WITH APU, THEN TRANSFERRED BLEEDS FROM BOTH ADJACENT ENGINES TO CROSS ENGINES IN REF. TO AMM36-10-00, WITH RESPECT TO AIR CONDITIONING SYS. NO NOTED DEFECTS AT THIS TIME. A/C OK'D FOR SVC.
2020
Part: STRINGER — CORRODED (BS 349-364) · airframe 36,680 hrs · 26,830 cycles
STRINGER 21R BETWEEN BS 349 - 364 WAS CORRODED. REPLACED THE STRINGER IAW SRM, AND DWG.
Part: FLOOR SUPPORT — CORRODED (BS 641-693) · airframe 36,680 hrs · 26,830 cycles
FLOOR SUPPORT, RBL 9, BS 641- 693 FOUND OUT OF LIMITS CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
Part: FLOOR SUPPORT — DAMAGED (BS 653) · airframe 36,680 hrs · 26,830 cycles
WHILE PERFORMING A MAJOR REPAIR ON THE FLOOR SUPPORT BETWEEN BS 477 TO 624 AT LBL 9, DAMAGE WAS FOUND AT BS 653, LBL 9. REPAIRED IAW SRM.
Part: STRINGER — CORRODED (BS 333-355) · airframe 36,680 hrs · 26,830 cycles
MAIN AVIONICS BAY STRINGER 27, BS 333 TO 355 HAD DEEP PITTING CORROSION AROUND RIVETS. REPLACED THE STRINGER IAW DWG, AND SRM.
Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 36,680 hrs · 26,830 cycles
TCAS ANTENNA DOUBLER, BS 295 TO 310 HAD SIGNS OF CORROSION. REPLACED THE TCAS ANTENNA DOUBLER IAW DWG, AND SRM.
Part: STRINGER — CORRODED (BS 333-349) · airframe 36,680 hrs · 26,830 cycles
STRINGER 26R, BETWEEN BS 333 AND 349 HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW DWG, AND SRM.
Part: STRINGER — CORRODED (BS 280-333) · airframe 36,680 hrs · 26,830 cycles
MAIN AVIONICS BAY STRINGER 23R CORRODED BETWEEN FS280.00 AND FS333. REPLACED THE STRINGER IAW DWG, AND SRM.
Part: FRAME — CORRODED (BS 295) · airframe 36,680 hrs · 26,830 cycles
BB 295 FRAME, BETWEEN STRINGERS 26L & 26R HAD SIGNS OF CORROSION. SPLICED IN A NEW FRAME SECTION IAW SRM.
Part: STRINGER — CORRODED (BS 280-333) · airframe 36,680 hrs · 26,830 cycles
MAIN AVIONICS BAY STR 22R CORRODED BETWEEN BS 280 AND 333. REPLACED THE STRINGER IAW DWG, AND SRM.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR MID DD3 INTERCOSTAL WAS CORRODED. REPLACED THE INDERCOSTAL IAW SRM AND DWG.
Part: SKIN — CORRODED (BS 980-988) · airframe 36,680 hrs · 26,830 cycles
EVALUATE EVIDENCE OF CORROSION ON EXTERIOR FUSELAGE BETWEEN FS 980 AND FS 988 AND BETWEEN STGR 26L AND STGR 26R. REPAIRED FUSELAGE SKIN BETWEEB FS 977 - 985 BETWEEN STGRS 26L - 26R, BY RERPLACING THE EXISTING DOUBLERS WITH NEW IAW REO. ALL CHECKED GOOD.
Part: SUPPORT — CORRODED (BS 310-333) · airframe 36,680 hrs · 26,830 cycles
CORROSION FOUND ON SILL BACKUP AT STRINGER 21L, BETWEEN BS 310 TO 333. REMOVED AND REPLACED THE SILL BACKUP DUE TO FOUND TO BE OUT OF LIMITS IAW SRM, DWG AND REO.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR ANGLE DD7A FWD OF BS 325 WAS CORRODED. INSTALLED A NEW ANGLE IAW SRM AND DWG.
Part: FORMER — CRACKED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR FORMER CRACKED AT BS 333. REMOVED AND INSTALLED A NEW PAX DOOR FORMER IAW SRM, AND DWG.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR AFT DD2 INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM, AND DWG.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR AFT DD5 INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR AFT DD7 INTERCOSTAL CRACKED. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG,
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR DD4 MID INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.
Part: STRINGER — CORRODED (BS 310-319) · airframe 36,680 hrs · 26,830 cycles
STRINGER 21R, BETWEEN BS 310 AND 319 WAS CORRODED. REPLACED THE STRINGER IAW DWG, SRM, AND DWG.
Part: INTERCOSTAL — DENTED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR FWD DD1 INTERCOSTAL DENTED IN RADIUS. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR DD2 MID INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.
Part: STRINGER — CORRODED (BS 310-333) · airframe 36,680 hrs · 26,830 cycles
STRINGER 20L, BS 310 TO 333 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE STRINGER IAW DWG, AND SRM.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR INTERCOSTAL DD7A AFT OF FS320 CORRODED. (C-CHECK) RO 8/5/2020 INSTALLED NEW INTERCOSTAL REF CRJ 700 SRM , AND DWG. COMPLIED WITH TASK CARD
Part: ANGLE — CRACKED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR ANGLE FS333 CRACKED. REMOVED AND INSTALLED A NEW PAX ANGLE IAW SRM AND DWG. RESTORED FINISH IAW SRM.
Part: FORMER — CRACKED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR FORMER FS329 CRACKED. INSTALLED A NEW FORMER IAW SRM AND DWG.
Part: COTTER PIN — MISSING (RT WING TE FLAP) · airframe 36,680 hrs · 26,830 cycles
RIGHT INBD FLAP, INBD ACTUATOR ASSY, FWD AND AFT LUG ASSEBLIES, THREE BOLTS MISSING COTTER PINS AND REMAINNG BOLT COTTER PIN DEFORMED BEYOND USE. VERIFIED TORQUE ON RT INBD FLAP, INBD HINGE ARM ASSY MOUNTING HARDWARE AND INSTALLED FOUR NEW COTTER PINS IAW AMM.
Part: RIVET — DAMAGED (RT WING TE FLAP) · airframe 36,680 hrs · 26,830 cycles
RIGHT OTBD FLAP, 2 SETS OF WORKING RIVETS IN CLOSE PROXIMITY TO EACH OTHER, ONE VERTICLE AND ONE HORIZONTAL. LOCATED ON TOP OF FLAP, SLIGHTLY OTBD OF CENTER ACTUATOR ASSY. REPLACED 15 RIVETS ON THE RT OTBD FLAP IAW REO.
Part: RIVET — DAMAGED (RT WING TE FLAP) · airframe 36,680 hrs · 26,830 cycles
RIGHT OTBD FLAP, 2 SETS OF WORKING RIVETS IN CLOSE PROXIMITY TO EACH OTHER, ONE VERTICLE AND ONE HORIZONTAL. LOCATED ON TOP OF FLAP, SLIGHTLY INBD OF INBD ACTUATOR ASSY. REPLACED 12 RIVETS ON THE RT OTBD FLAP IAW REO.
Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 36,680 hrs · 26,830 cycles
INTERCOSTAL AT STRINGER 20R, BETWEEN BS 310 AND 319 HAD CORROSION AT MULTIPLE LOCATIONS. THE INTERCOSTAL IS EXFOLIATED 100%, ORIGINAL MATERIAL THICKNESS IS .063" AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG, AND SRM.
Part: STRINGER — CORRODED (BS 295-310) · airframe 36,680 hrs · 26,830 cycles
STRINGER 19R, BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER IAW SRM, DWG, AND REO.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 36,680 hrs · 26,830 cycles
THE BS 280 FLOORBEAM ANGLE HAD CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE ANGLE IAW SRM.
Part: STRINGER — CORRODED (BS 295-333) · airframe 36,680 hrs · 26,830 cycles
STRINGER 20L FROM BS 295 TO 333 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND INSTALLED A NEW STRINGER IAW DWG, AND SRM.
Part: SEAT TRACK — CORRODED (BS 693-830.4) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK, BS 693 - 830.4, LBL 9 HAD CORROSION. REPLACED THE SEAT TRACK IAW AMM.
Part: FLOOR SUPPORT — CORRODED (BS 477-565) · airframe 36,680 hrs · 26,830 cycles
FLOOR SUPPORT CAP JUST AFT OF BS 565 TO 477, RBL 9 HAD CORROSION. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM.
Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK, RBL 9, BS 349 - 477 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.
Part: STRINGER — CORRODED (BS 295-310) · airframe 36,680 hrs · 26,830 cycles
STRINGER 19L, BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER WITH NEW IAW REO.
Part: CUP — CORRODED (DOOR HANDRAIL) · airframe 36,680 hrs · 26,830 cycles
* THE PAX DOOR INTERNAL SURROUND FUSELAGE SIDE FWD HANDRAIL CUP HAS CORROSION. REMOVED CORROSION FROM PAX DOOR SURROUND FWD. CLOSING FITTING (HANDRAIL CUP). IAW SRM. FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW IAW SRM. RESTORED FINISH IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 549-565) · airframe 36,680 hrs · 26,830 cycles
LEFT FLOOR SUPPORT BETWEEN BS 549 TO 565 HAD THREE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND DWG.
Part: STRINGER — CORRODED (BS 1015-1047) · airframe 36,680 hrs · 26,830 cycles
STRINGER 26R, BS 1015 TO 1047 HAD CORROSION. REPLACED THE STRINGER IAW SRM AND DWG.
Part: GUSSET — CORRODED (BS 364) · airframe 36,680 hrs · 26,830 cycles
THE INTERNAL SURROUND STRUCTURE, FUSELAGE SIDE OF THE AVIONICS BAY DOOR FWD GUSSET AT BS 364, STRINGER 25L HAD CORROSION. BLENDED THE CORROSION IAW SRM, INSTALLED A NEW GUSSET IAW DWG, AND SRM.
Part: STRUCTURE — CORRODED (BS 280-333) · airframe 36,680 hrs · 26,830 cycles
* THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION REF CRJ700 SRM FROM THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 AT MULTIPLE LOCATIONS OF CORROSION. FOUND MULTIPLE ELONGATED HOLES, REPAIRED REF REO.
Part: STRINGER — CORRODED (BS 295-310) · airframe 36,680 hrs · 26,830 cycles
* A BAY - STGR 22L - BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER IAW DWG, AND SRM.
Part: FLOOR SUPPORT — CORRODED (BS 477-565) · airframe 36,680 hrs · 26,830 cycles
FLOOR SUPPORT CAP FROM JUST AFT OF FS 565.0 TO FS 477.0 LBL 9 HAD CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM, AND REO.
Part: FRAME — CORRODED (BS 1015) · airframe 36,680 hrs · 26,830 cycles
FWD SIDE OF FRAME AT FS 1015 STRINGERS 26L TO 27, HAD CORROSION. PERFORMED A SPLICE REPAIR TO THE FRAME IAW REO.
Part: SEAT TRACK — CORRODED (BS 364-477) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK, LBL 27, BS 364 - 477 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 485-693) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK, RBL 9, BS 485 - 693 HAD CORROSION. REPLACED THE SEAT TRACK SECTION IAW AMM.
Part: SEAT TRACK — CORRODED (BS 693) · airframe 36,680 hrs · 26,830 cycles
CORROSION ON SEAT TRACK CAP FS 693, RBL 9. PERFORMED REPAIR TO THE SEAT TRACK IAW REO.
Part: SEAT TRACK — CORRODED (BS 693-830.4) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK, BS 693 TO 830.4, RBL 9 HAD CORROSION. REPLACED THE SEAT TRACK IAW AMM.
Part: STRUCTURE — CORRODED (BS 280) · airframe 36,680 hrs · 26,830 cycles
* A BAY - AFT OF FS 280 - STGR'S 18 - 21L- JOINT PLATE CORRODED. REMOVED CORROSION FROM FS280 JOINT PLATE BETWEEN STGRS 18L - 21L, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS REF REO.
Part: FLOOR SUPPORT — CORRODED (BS 565-693) · airframe 36,680 hrs · 26,830 cycles
FLOOR SUPPORT CAP FROM FS 693.0 TO JUST AFT OF FS 565.0 AT LBL 9 HAD CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM, AND REO.
Part: FLOOR SUPPORT — CORRODED (BS 565-693) · airframe 36,680 hrs · 26,830 cycles
FLOOR SUPPORT JUST FWD OF BS 693 TO JUST AFT OF BS 565, RBL 9 HAD CORROSION. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM.
Part: CROSSBEAM — CORRODED (BS 333) · airframe 36,680 hrs · 26,830 cycles
* THE CROSSBEAM CAP AT BS 333, LBL 27 HAD CORROSION. PERFORMED A REPAIR TO THE CROSSBEAM IAW REO. COMPLIED WITH TASK CARD.
Part: HINGE — GOUGED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PAX DOOR HINGE FUSELAGE SIDE HAS NEW GOUGE ON AFT LUG LANDING. REMOVED THE GOUGE FROM PAX DOOR HINGE AFT LUG LANDING, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO. NO FURTHER DEFECTS NOTED. COMPLIED WITH TASK CARD.
Part: SEAT TRACK — CORRODED (BS 953-989) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK SECTION AT RBL 9, BS 953 - 989 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 830.4-953) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK SECTION AT RBL 9, BS 830.4 - 953 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.
Part: SEAT TRACK — CORRODED (BS 830.4-953) · airframe 36,680 hrs · 26,830 cycles
SEAT TRACK SECTION, LBL 9, BS 830.4 - 953 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.
Part: HINGE — GOUGED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PASSENGER DOOR HINGE, SECOND LUG FROM FORWARD SIDE WAS GOUGED. REMOVED THE GOUGES FROM PAX DOOR HINGE SECOND LUG, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO. NO FURTHER DEFECTS NOTED. COMPLIED WITH TASK CARD.
Part: STOP FITTING — CHAFED (GALLEY DOOR) · airframe 36,680 hrs · 26,830 cycles
THE GALLEY SERVICE DOOR EXTERNAL SURROUND FUSELAGE SIDE ALL STOP FITTINGS ARE CHAFED. PERFORMED REPAIR OF THE GALLEY SERVICE DOOR EXTERNAL SURROUND FUSELAGE SIDE STOP FITTINGS IAW REO.
Part: FITTING — GOUGED (LT MLG) · airframe 36,680 hrs · 26,830 cycles
LEFT MLG SIDE STAY FITTING WAS GOUGED WITH RAISED METAL FROM CONTACT WITH SIDE STAY PINTLE NUT COTTER PIN. REMOVED THE DAMAGE FROM THE LT MLG SIDE STAY FITTING IN AREA ABOVE PINTLE PIN NUT IAW SRM. DAMAGE REMOVAL MEASURES 1.090"" LONG BY .980"" WIDE BY .016"" DEEP.
Part: FORMER — CORRODED (PAX DOOR) · airframe 36,680 hrs · 26,830 cycles
PASSENGER DOOR, FWD FORMER CORRODED AROUND LOWER TENSION TIE. REMOVED AND INSTALLED A NEW PAX DOOR FWD FORMER IAW SRM, AND DWG. NO LEAKS NOTED.
Part: PANEL — CHAFED (LT NACELLE) · airframe 36,680 hrs · 26,830 cycles
*LH ENGINE UPPER FAN COWL PANEL 432AT IS CHAFFED ON INNER SKIN AND STIFFENER. LH ENGINE UPPER FAN COWL INNER SKIN BLENDED AND FOUND WITHIN LIMITS IAW SRM. STIFFENER REPAIRED IAW SRM.
Part: RETAINER — GOUGED (CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
THE FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE AFT SEAL RETAINER LOWER END WAS GOUGED. THE SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM.
Part: STOP FITTING — CHAFED (E/E BAY DOORWAY) · airframe 36,680 hrs · 26,830 cycles
THE MAIN AVIONICS BAY DOOR EXTERNAL FUSELAGE SURROUND FWD LT STOP FITTING WAS CHAFED. NO DAMAGE ALLOWED TO THE STOP FITTING. REMOVED THE STOP FITTING. LOCATED AND DRILLED A NEW FITTING IAW SRM. INSTALLED THE NEW FITTING IAW AMM.
Part: STOP FITTING — CHAFED (FWD CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
THE FWD CARGO DOOR FWD LOWER STOP WAS CHAFED. REMOVED AND REPLACED THE STOP FITTING IAW AMM. OPS TEST GOOD
Part: STOP FITTING — CHAFED (E/E BAY DOORWAY) · airframe 36,680 hrs · 26,830 cycles
THE MAIN AVIONICS BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD RT STOP FITTING WAS CHAFED. NO DAMAGE ALLOWED TO THE STOP FITTING. REMOVED AND REPLACED THE STOP FITTING IAW SRM AND AMM.
Part: STOP FITTING — CHAFED (FWD CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
* THE FWD CARGO DOOR FWD UPPER STOP IS CHAFED. REMOVED AND REPLACED THE FWD CARGO DOOR FWD UPPER STOP BOLT AND JAM NUT IAW AMM. OPS TEST GOOD
Part: RETAINER — GOUGED (FWD CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
THE FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD SEAL RETAINER LOWER END IS GOUGED. FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD SEAL RETAINER FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED WITH NEW SEAL RETAINER IAW SRM.
Part: STOP FITTING — CHAFED (FWD CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
THE FWD CARGO DOOR AFT LOWER STOP IS CHAFED. REMOVED AND REPLACED FWD CARGO DOOR STOP FITTING IAW AMM.
Part: STOP FITTING — CHAFED (FWD CARGO DOOR) · airframe 36,680 hrs · 26,830 cycles
THE FWD CARGO DOOR AFT UPPER STOP WAS CHAFED. REMOVED AND REPLACED THE STOP FITTING IAW AMM. OPS TEST GOOD
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 36,680 hrs · 26,830 cycles
LEFT INBD FLAP LOWER SURFACE HAS DENTS. REPAIRED DENTS ON THE LT INBD FLAP, LOWER SURFACE IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 36,680 hrs · 26,830 cycles
RIGHT INBD FLAP LOWER SURFACE HAD TWO DENTS. REPAIRED THE FLAP LOWER SURFACE DENTS IAW SRM.
2018
Part: SKIN — DENTED (BS 1162) · airframe 32,585 hrs · 23,475 cycles
LOWER SKIN DENTED JUST AFT OF BS 1162, BETWEEN STRINGERS 24R AND 25R. INSTALLED A DOUBLER IAW REO.
Part: SKIN — CHAFED (LT AILERON) · airframe 32,585 hrs · 23,475 cycles
LEFT AILERON ALONG THE TOP LEADING EDGE WAS CHAFED. BLENDED THE CHAFE IAW REO.
Part: SKIN — DENTED (BS 549) · airframe 32,585 hrs · 23,475 cycles
FOUND A DENT JUST FWD OF BS 549 JUST BELOW STRINGER 16L. DRESSED DENT BACK TO CONTOUR IAW REO. NO LEAKS NOTED.
Part: SKIN — DENTED (FUSELAGE) · airframe 32,585 hrs · 23,475 cycles
DENT FOUND ON BOTTOM FUSELAGE SKIN APPROXIMATELY 30 INCHES AFT OF AEB DOOR. INSTALLED A DOUBLER IAW REO.
Part: FRAME — CRACKED (BS 235) · airframe 32,585 hrs · 23,475 cycles
LEFT FRAME AT BS 235 FOUND CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM.
2017
Part: STRINGER — CRACKED (BS 280) · airframe 3 hrs · 22,376 cycles
STRINGER 3L CRACKED BS 280. COMPLIED WITH EC/TC SB 670BA-53-040 01, SB 670BA-53-040 01, EC/TC REO 670-53-21-493, AND REO 670-53-21-493.
Part: SKIN — DENTED (LT WING LE SLAT) · airframe 31,160 hrs · 22,376 cycles
TWO DENTS FOUND ON THE LT WING SLAT 3 AT SS 407.75. CORRECTIVE ACTION: DENT ON LH WING SLAT 3 SS407.75 REPAIRD IAW REO 670-57-42-720 AND ECTC REO670-57-42-720. ALL DEFECTS CORRECTED.
Part: STRINGER SPLICE — CORRODED (BS 295-310) · airframe 31,160 hrs · 22,376 cycles
STRINGER SPLICE 24R HAS CORROSION BETWEEN BS 295 - 310. REMOVED AND REPLACED THE STRINGER AND SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-32420.
Part: SKIN — CORRODED (BS 364) · airframe 31,160 hrs · 22,376 cycles
AVIONICS BAY DOOR SURROUND SKIN HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-21-242, REO 670-53-21-242, AND MODSUM IS67053210097.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,160 hrs · 22,376 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED. COMPLIED WITH EC/TC REO 670-51-11-072, AND REO 670-52-11-072.
Part: PANEL — CRACKED (PAX DOOR) · airframe 31,160 hrs · 22,376 cycles
TWO CRACKS ON AFT. PAX DOOR SIDE PANEL. COMPLIED WITH SRM 52-11-04-201-004-A01, AND TR 52-0025.
Part: BUTT JOINT — CORRODED (BS 280) · airframe 31,160 hrs · 22,376 cycles
BS 280 BUTT STRAP HAS CORROSION STRINGERS 27 - 26R.. COMPLIED WITH EC/TC EA 30-2017-097 AND EA 30-2017-097.
Part: LONGERON — CORRODED (BS 333-349) · airframe 31,160 hrs · 22,376 cycles
CORROSION ON STRINGER 25R BS 333 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-32050.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 31,160 hrs · 22,376 cycles
STRINGER SPLICE 25L HAS CORROSION AROUND BS 333. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-32420.
Part: STRINGER — CORRODED (BS 333-364) · airframe 31,160 hrs · 22,376 cycles
CORROSION ON STRINGER 25L, BS 333 - 364. REMOVED AND REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-32050.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL AT FS 713-761 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-013 AND REO 670-53-00-013.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
STR 25R SPLICE JOINT AT FS 333.00 CORRODED. REMOVED AND REPLACED SPLICE JOINT AT FS 333.00 AND STR 25R PER SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND DRWING SH670-32420.
Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.
Part: DOUBLER — CHAFED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FS 977 CHAFFED ON PREVIOUS REPAIR ON BELLY. COMPLIED WITH EXPRESS ECTC REO 670-53-00-507 AND REO 670-53-00-507. ALL DEFECTS CORRECTED.
Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.
Part: STEP — CORRODED (PAX DOOR) · airframe 31,160 hrs · 22,376 cycles
PAX DOOR STEP PANEL 832AT HAS CORROSION. REMOVED CORROSION, REPAIRED DOOR STEP PANEL BY COMPLYING WITH EC/TC EA 30-2017-096 AND EA 30-2017-096.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL AT FS 713-761 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT TRACK AT FS 501-581 LBL9 IS CORRODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 FOR REPLACEMENT OF SEAT TRACK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL AT FS 785-855 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
STRINGER 25L HAS CORROSION 319-349. REMOVED AND REPLACED STRINGER 25L AT FS 319.00-349.00 IAW SRM 51-42-06-001-001-A01,51-40-11-001-001-A01 AND DRAWING SH670-31212.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
STRINGER 25R HAS CORROSION BETWEEN FS 280-310. REMOVED AND REPLACED STRINGER 25R AT FS 280-333 IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-31212.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT TRACK AT FS 581- 685 LBL9 IS CORRODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 FOR REPLACEMENT OF SEAT TRACK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT TRACK AT FS 581-685 RBL9 IS CORRODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 FOR REPLACEMENT OF SEAT TRACK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT RAIL FS 685-690 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL AT FS 869-961 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT TRACK AT FS 501-581 RBL9 IS CORRODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 FOR REPLACEMENT OF SEAT TRACK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL AT FS 785-856 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-013 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLOOR SEAT TRACK AT FS 372-501 LBL9 IS CORRODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 FOR REPLACEMENT OF SEAT TRACK.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
STRINGER 26R BETWEEN FS 280-333 HAS CORROSION. REMOVED AND REPLACED STRINGER 26R FS 280.00-333.00 IAW SRM 51-42-06-001-001-A01 AND 51-42-001-001-A01. AND DRAWING SH670-31634 .
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
FLT COMPARTMENT ENTRY SUPPORT ANGLE CORRODED FS 280.00. REMOVED AND REPLACED SUPPORT ANGLE FS 280.00 IAW SRM 51-42-06-001-001 AND DRAWING CC670-34191.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL FS 575-675 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL FS 675-713 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL FS 379-485 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL FS 675-713 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL AT FS 485-575 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL AT FS 379-485 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
PACKER HAS CORROSION RBL9 FS 333. REMOVED AND REPLACED PACKER P/N SH670-32167-3 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32120.
Part: FRAME — CRACKED (BS 333) · airframe 31,160 hrs · 22,376 cycles
FRAME BS 333 CRACKED NEAR STR 1R. REPAIRED THE FRAME IAW REO 670-53-21-1441, AND EC/TC REO 670-53-21-1441, REV A. THIS IS A MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
LT SIDE SEAT RAIL FS 575-675 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 22,376 cycles
RT SIDE SEAT RAIL AT FS 485-575 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.
Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 30,630 hrs · 25,713 cycles
PILOT REPORTED ON LANDING, THE BRAKENG WAS ASYMETRIC WITH ACFT PULLING RIGHT AT GATE. LEFT INBD BTMS SHOWED 00 AND LT INBD BRAKE WAS COLD TO TOUCH. MX REMOVED AND REPLACED THE LT INBD WHEEL SPEED TRANSDUCER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,169 hrs · 21,638 cycles
DURING SCHEDULED MX INSPECTION, THE ROW 17 OVERHEAD EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT BULB OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
2016
Part: LENS — MISSING (EXIT SIGN) · airframe 28,707 hrs · 20,514 cycles
EMERGENCY EXIT SIGN COVER MISSING FROM GALLEY NR 2. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-00. ACFT OK FOR SERVICE.
Part: LIGHT — MISSING (CABIN) · airframe 28,629 hrs · 20,446 cycles
GALLEY FLOOR TRACK LIGHT MISSING. INSTALLED MISSING EMERGENCY LIGHT STRIP IN GALLEY IAW AMM 33-57-01.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,326 hrs · 20,210 cycles
BULB BURNED ON ENTRANCE DOOR LOWER EXIT LIGHT. R & R LIGHT IAW AMM 33-51-05, OPS CHECK GOOD.
Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 28,023 hrs · 19,966 cycles
CARGO DOOR THRESHOLD CORRODED. REPLACED IAW SRM 53-61-23-101-001-A01.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 28,023 hrs · 19,966 cycles
CORROSION FOUND ON LBL 27, FS 1031 FLOORBEAM. REPAIRED THE FLOORBEAM IAW SRM 53-61-43-101-001-A01.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 28,023 hrs · 19,966 cycles
CORROSION FOUND ON LBL 9, FS 1031 FLOORBEAM. REPAIR THE FLOORBEAM IAW SRM 53-61-43-101-001-A01.
2015
Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 27,745 hrs · 19,762 cycles
F/A REAR MEGAPHONE NOT WORKING. TIGHTENDED R2 BATTERIES AS REQUIRED IAW GMM 3-8.6.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 27,288 hrs · 19,422 cycles
LIGHTED PLACARD AT SERVICE DOOR PLACARD MISSING. INSTALLED SERVICE DOOR COVER IAW AMM 33-51-00.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 26,329 hrs · 18,622 cycles
SERVICE DOOR EXIT SIGN CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE DOOR EXIT SIGN COVER LENS IAW AMM TASK 33-51-05-000, 400,-801-A01, OPS CHECKED GOOD.
Part: SHEAR TIE — CORRODED (BS 349) · airframe 26,329 hrs · 18,622 cycles
CLEAT PN SH670-37014-1 ON RT INTERCOSTAL AT FS 349 IS CORRODED BEYOND LIMITS. COMPLIED WITH SNIEO SH670-32014, SN 02 AS WRITTEN. RECEIVED ECTC SNIEO- 32014 501 FABRICATED AND INSTALLED ANGLE, PN 51-670-32014-1 IAW SNIEO 670-32015 501.
Part: DOUBLER — CORRODED (BS 349) · airframe 26,329 hrs · 18,622 cycles
DOUBLER ON RT INTERCOSTAL AT BS 349 CORRODED BEYOND LIMITS. COMPLIED WITH DOUBLER FABRICATION IAW SNIEO SH670-32003501. FABRICATED AND INSTALLED DOUBLER IAW SNIEO 670-320003 S01 501.
Part: STRINGER — CORRODED (BS 319-349) · airframe 26,329 hrs · 18,622 cycles
STR 20R HAS EXFOLIATION CORROSION ON FLANGES BETWEEN FS 319.70 AND FS 349.00. REMOVED STR 20R SEGMENT BETWEEN FS 319.70 AND FS 349.00 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. PICKED UP ALL ATTACHING HOLES IN STR 20R, REF SRM 51-40-11-001-001 & DWG SH670-32420. INSTALLED STR 20R BETWEEN FS 319 AND FS 349 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-32420.
Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 26,329 hrs · 18,622 cycles
SERVICE DOOR SEAL STRIKER CORRODED. REMOVED SERVICE DOOR SEAL STRIKER IN REF TO SRM 51-42-06-001-001 A01. INSTALLED NEW SERVICEABLE SERVICE DOOR SEAL STRIKER IN REF TO SRM 51-42-06-001-001-A01.
Part: STRAP — DAMAGED (RT WING) · airframe 26,329 hrs · 18,622 cycles
OVERSIZE HOLE, RT WING STRAP IAW RNC. RECEIVED REO 670-21-775 REPAIR TO LOWER WING ASSY P1 DATED 2015-04-22. COMPLIED WITH REO 670-57-21-775 P1 DATED 2015-04-22. RECEIVED PERMANENT REO 670-57-21-775 REV-- DATED 2015-04-26 AND REQUESTED EC/TC. RECEIVED AND COMPLIED WITH ECTC REO 670-57-21-775.
Part: BLANKING PLATE — CORRODED (SERVICE DOOR) · airframe 26,329 hrs · 18,622 cycles
BLANKING PLATE AT BS 349-364, RT HAS CORROSION, SERVICE DOOR. REMOVED CORROSION ON BLANKING PLATE AT FS 349-364 RT IN REF TO SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV, DATED 01/22/2014 AS WRITTEN.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 26,329 hrs · 18,622 cycles
UPPER ANGLE AT PAX DOOR HAS CORROSION. SEVERE CORROSION IS OUT OF LIMITS IAW CRM 53-21-23-101-001-A01. R & R UPPER MIDCAP ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-41-02-001-001-A01 AND DWG SH670-31825.
Part: STRUCTURE — CORRODED · airframe 26,329 hrs · 18,622 cycles
SERVICE DOOR WEB FLOOR PROTECTORS HAVE CORROSION 3. 3 EA FLOOR PROTECTORS ARE CORRODED OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED 4 EA FLOOR PROTECTORS AT SERVICE DOOR IN REF TO SRM 51-42-06-001-001-A01. INSTALLED 3EA NEW FLOOR PROTECTORS, REINSTALLED 1EA FLOOR PROTECTOR PREVIOUSLY REMOVED IN REF TO SRM 51-42-06-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 26,329 hrs · 18,622 cycles
RIGHT FLOOR SUPPORT AT BS 280 - 319.7 HAS CORROSION. REMOVED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01. INSTALLED IAW SRM 51-42-13-001-001-A01, 51-42-06-001-001-A01 AND 51-45-00-001-001-A01.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 26,329 hrs · 18,622 cycles
LOWER ANGLE AT PAX DOOR HAS CORROSION. SEVERE CORROSON IS OUT OF LIMITS IAW CRJ 53-21-23-101-001-A01. R & R LOWER PAX DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31875.
Part: ANGLE — CORRODED · airframe 26,329 hrs · 18,622 cycles
GALLEY DOOR FLOOR PROTECTOR ANGLES HAS CORROSION, 4. REMOVED 4 EA GALLEY DOOR FLOOR SUPPORT ANGLES IN REF TO SRM 51-42-06-001-001-A01. INSTALLED 4 EA NEW GALLEY DOOR FLOOR SUPPORT ANGLES IN REF TO SRM 51-42-06-001-001-A01.
Part: PLATE — CORRODED (SERVICE DOOR) · airframe 26,329 hrs · 18,622 cycles
SERVICE DOOR JOINT PLATE HAS CORROSION. R & R SERVICE DOOR FWD FITTING IN REF TO SRM 51-42-21-001-001-A01.
Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 26,329 hrs · 18,622 cycles
LOWER ANGLE SILL AT SERVICE DOOR HAS CORROSION. SEVERE CORROSION OUT OF LIMITS IAW SRM NO DAMAGE ALLOWED AROUND FASTENERS 53-21-23-101-002-A01. REMOVED LOWER ANGLE SILL AT SERVICE DOOR IN REF TO SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE LOWER ANGLE SILL AT SERVICE DOOR IN REF TO SRM 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 26,329 hrs · 18,622 cycles
UPPER ANGLE AT SERVICE DOOR HAS CORROSION, SEVERE CORROSION IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED UPPER ANGLE IAW SRM 51-42-06-001-001-A01, 7 51-42-21-001-001-A01 AND INSTALLED IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 26,324 hrs · 18,617 cycles
RIGHT SIDE FLOOR SEAT TRACK CORRODED AT BS 349 - 485. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 377-708) · airframe 26,324 hrs · 18,617 cycles
LT SIDE SEAT TRACK CORRODED AT BS 677 - 708 SIDE WALL. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 893-969) · airframe 26,324 hrs · 18,617 cycles
RIGHT SIDEWALL SEAT TRACK CORRODED AT BS 893 - 969. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: INTERCOSTAL — CORRODED (BS 319-349) · airframe 26,324 hrs · 18,617 cycles
INTERCOSTAL BETWEEN BS 319-349 STR 20R HAS CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED INTERCOSTAL AT STR 20R BETWEEN BS 319 - 349 IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001 & DWG SH670-31950. DRILL UP & INSTALL SERVICEABLE INTERCOSTAL & ATTACH ANGLES REF DWG SH670-31950. PICKED UP ATTACH HOLES FOR INTERCOSTAL & ATTACH ANGLES REF SRM 51-40-11-001-001, DWG SH670-31950. INSTALLED SERVICEABLE DOUBLER IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 26,329 hrs · 18,622 cycles
RT SIDE WALL SEAT TRACK CORRODED AT BS 708 - 761.85. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND AMM 53-00-49-00-400-801, A03.
Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,329 hrs · 18,622 cycles
BS 280 WEB ANGLE CRACKED AT RBL 26. R & R ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 26,329 hrs · 18,622 cycles
LEFT SIDE SEAT TRACK CORRODED AT BS 677 - 708. CORROSION OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 26,329 hrs · 18,622 cycles
RIGHT SIDE WALL SEAT TRACK CORRODED AT FS 565 - 677. CORROSION IS OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND REPLACED IAW AMM 53-00-49-400-801-A03.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 26,329 hrs · 18,622 cycles
RIGHT COCKPIT FLOORBEAM IS CRACKED. RECEIVED AND COMPLIED WITH ECTC REO 670-53-11-896 AND REO 670-53-11-896, REV DATED 03-17-2015 AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 26,329 hrs · 18,622 cycles
RIGHT SIDE SEAT TRACK CORRODED AT BS 485 - 565. CORROSION OUT OF LIMITS IAW SRM 53-31-49-11-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 26,324 hrs · 18,617 cycles
LEFT SIDE SEAT TRACK CORRODED AT BS 485 - 565, SIDE WALL. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 26,324 hrs · 18,617 cycles
LEFT SIDE SEAT TRACK CORRODED AT BS 708 - 761.85 SIDE WALL. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND AMM 53-00-49-00-400-801, A03.
Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,329 hrs · 18,622 cycles
BS 280 WEB ANGLE CRACKED AT LBL 26. REMOVED CRACKED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 26,329 hrs · 18,622 cycles
LT SIDE WALL SEAT TRACK CORRODED AT BS 785.15 - 863. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,324 hrs · 18,617 cycles
BS 280 FWD FLOORBEAM ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. FLOORBEAM ANGLE AT BS 280 R & R IAW SB 670BA-53-041.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,323 hrs · 18,616 cycles
F/S 280, FLOORBEAM RT SIDE CORRODED. FLOORBEAM R & R IAW SB 670BA-53-041.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 26,324 hrs · 18,617 cycles
F/S 280 BULKHEAD WEB RT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV DATED 04/27/2011.
Part: FRAME — CORRODED (BS 319) · airframe 26,324 hrs · 18,617 cycles
FRAME AT BS 319 BETWEEN 26L-26R FWD SIDE HAS CORROSION. REMOVED CORROISON BS 319 BETWEEN STR 26L AND STR 26R ON FRAME ATTACH FLANGE, WEB, AND RADIUS IAW SRM 51-21-06-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 26,324 hrs · 18,617 cycles
BS 280, BULKHEAD WEB LT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV DATED 04/27/2011.
Part: FITTING — CORRODED (BS 280-265) · airframe 26,324 hrs · 18,617 cycles
FWD SOCK FITTING BETWEEN FRAMES 280 AND 265 LT INTERCOSTAL CORRODED LOWER FLANGE. BLENDED NOSE JACK FITTING LT INTERCOSTAL REF SRM 51-21-06-001-001. COMPLIED WITH EA 32-2015-180.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,324 hrs · 18,617 cycles
BS 280 FLOORBEAM, LT SIDE CORRODED. FLOORBEAM R & R IAW SB 670BA-53-041.
Part: FRAME — CORRODED (BS 310) · airframe 26,323 hrs · 18,616 cycles
FRAME AT FS 310 BETWEEN STR 26L-26R FWD SIDE HAS CORROSION. REMOVED CORROSION AT FS 310, FRAME ATTACH ANGLE RADIUS, AND WEB FROM STR 26L TO 26R IAW SRM 51-21-06-001-001-A01. RECEIVED EA 32-2015-158 AND COMPLIED WITH EA 32-2015-158.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,323 hrs · 18,616 cycles
INTERCOSTAL AT BS 349-364, STR 26R HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED DAMAGED INTERCOSTAL AT STR 26R BETWEEN FS 349-364. INSTALLED NEW INTERCOSTAL IAW DWG, SH670-32075, REV A AND SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,323 hrs · 18,616 cycles
CRAWLWAY FLOOR SUPPORT ANGLE AT FS 280 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT LIMITS IAW SRM 53-00-00-101-001-A01. R & R DAMAGED FLOOR SUPPORT ANGLE AT FS 280 WITH A NEW SERVICEABLE ANGLE IN REF TO SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: STRAP — CORRODED (BS 280) · airframe 26,323 hrs · 18,616 cycles
F/S 280 CIRCUMFERENTIAL STRAP BETWEEN STR 22L-21R HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FS 280 BUTT STRAP FROM STR 26L-26R. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED REMAINING CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FS 280 BUTT STRAP FROM STR 26R-24R FOR CORROSION 51-21-06-001-001-A01. REMOVED CORROSION FS 280 BUTT STRAP FROM STR 24R TO 21R IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FS 280 BUTT STRAP FROM STR 26L TO 22L IAW SRM 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH EA 32-2015-157. RECEIVED AND COMPLIED WITH ECTC EA 32-2018-157.
Part: FRAME — CORRODED (BS 333) · airframe 26,323 hrs · 18,616 cycles
FRAME AT BS 333 BETWEEN STR 27-26L HAS CORROSION FWD SIDE REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 & 53-21-06-101-002-A01. REMOVED CORROSION ON F/S 333.00 BETWEEN STRG 27-26L, REF: SRM 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH EA 32-2015-166.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,323 hrs · 18,616 cycles
INTERCOSTAL AT BS 349 - 364, STR 27R HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED DAMAGED INTERCOSTAL. INSTALLED NEW INTERCOSTAL AT STR27R BETWEEN FS 349-364 IAW DWG SH670-32075, REV A AND SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,323 hrs · 18,616 cycles
INTERCOSTAL AT BS 349-364, STR 27L HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED INTERCOSTAL AT STR 2L BETWEEN FS 349-364 BEGAN INSTALLED NEW INTERCOSTAL REF: DWG SH670-32075, REV A SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: FRAME — CRACKED (BS 193) · airframe 26,323 hrs · 18,616 cycles
AT FRAME BS 193, THE FLOOR OF THE FORWARD EQUIPMENT COMPARTMENT IS CRACKED. COMPLIED WITH EC/TC REO 670-53-11-509 AND REO 670-53-11-509, REV B, DATED 01-28-2014.
Part: LIGHT — WRONG PART (CABIN) · airframe 26,323 hrs · 18,616 cycles
CABIN FLOOR LIGHTING STRIPS HAVE SMALL PIECES INSTALLED THROUGH OUT CABIN FOUND DURING INTERIOR INCOMING CHECK. REPLACED SMALL FLOOR PATH LIGHTING STRIPS WITH LONGER STRIP IAW AMM TASK 33-51-01-400-801 A04 AND AMM SUPP 33-51-01, REV A.
Part: ANGLE — CRACKED (BS 1144-1162) · airframe 26,323 hrs · 18,616 cycles
CLIP ON RT SIDE AT STR 9R BETWEEN BS 1144 - 1162 IS CRACKED IN HALF. R & R CLIP IAW SRM 51-42-06-001-001-A01.
Part: PAINT — SCRATCHED (FUSELAGE) · airframe 26,329 hrs · 18,622 cycles
PAINT SCRATCHED OFF ABOVE FWD CARGO DOOR. COMPLIED WITH EC/TC EA -32-2015-163 PERMANENT REPAIR. REMOVED SCRATCH IAW SRM TE 51-0050. NO DAMAGE ALLOWED IAW SRM 53-31-01-101-002-A01. RECEIVED AND COMPLIED WITH ECTC EA 32-2015-163.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 26,092 hrs · 18,438 cycles
F/A FRONT FLASHLIGHT INOPERATIVE. R & R F/A FRONT FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD PLACARD REMOVED.
2014
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,574 hrs · 18,056 cycles
PAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE MOTOR ASSIST PULLEY BRACKET. FABRICATED A NEW ANGLE SECTION. SEALED AND WET INSTALLED THE DRAG ANGLE IAW SRM 52-11-04, REPAIR 002-A01. MAJOR REPAIR IAW GMM 5-3.
Part: HANDLE — GOUGED (CARGO DOOR) · airframe 24,964 hrs · 17,579 cycles
AFT CARGO DOOR EXTERIOR HANDLE GOUGED. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 52-31-01. BLENDED DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00 IAW EA 25-2014-272. RESTORED SURFACE FINISH TO THE BLEND OUT AREA IAW SRM 51-21-16 IAW EA 25-2014-272.
2013
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 23,247 hrs · 16,305 cycles
F/A MEGAPHONE IS INOPERATIVE. R & R MEGAPHONE, IAW AMM 25-61-14, OPS CHECKED GOOD.
Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 21,942 hrs · 15,355 cycles
ROW 4 AND 7 CEILING AND LT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,926 hrs · 15,345 cycles
LEFT EXTERIOR EMERGENCY LIGHT NR 6 OUT. RELAMPED THE LT EXTERIOR EMERGENCY LIGHT NR 6 AND OPS CHECKED GOOD IAW AMM 33-51-00.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 21,806 hrs · 15,263 cycles
EMERGENCY LIGHTS NOT WORKING. CHARGED SYS, DISCREPANCY NO LONGER EXISTS IAW MCC, NO FURTHER ACTION IS REQUIRED.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 21,450 hrs · 15,012 cycles
PAX DOOR HAS CRACKED INTERCOSTAL INSIDE ACCESS PANEL 832BR. REMOVED CRACKED INTERCOSTAL INSIDE ASD INSIDE ACCESS PANEL 832BR IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01. DRILLED UP NEW INTERCOSTAL INSIDE ACCESS PANEL (832BR) ON ASD IAW SRM 700 51-40-11-001-001-A01. INSTALLED INTERCOATAL IAW SRM 51-42-06-001-001-A01 AN 51-42-21-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 21,495 hrs · 15,045 cycles
RT SIDE OF FWD EQUIPMENT BAY FLOOR IS CRACKED BY ADG PUMP. REPAIRED IAW REO 670-53-11-509.
2012
Part: TIRE — LOW PRESSURE (NLG) · airframe 20,920 hrs · 14,626 cycles
NLG STEERING INOPERATIVE MESSAGE IN FLIGHT, NOSE WHEEL EXCESSIVE SHIMMY ON TAXI AND TAKEOFF. EMERGENCY DECLARED. FOUND LT AND RT NOSE TIRE PRESSURE LOW, SERVICED TIRE TO 154 PSI TORQUED NOSE TIRES IAW AMM 32-41-00 PERFORMED SYS RESET IAW FIM 32-50-00 OF NOSE WHEEL STEERING SYS OPS CHECK GOOD. SDR CLOSED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,355 hrs · 13,469 cycles
LEFT EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHT LAMP INOPERATIVE. RELAMPED. OPS CHECKED GOOD IAW AMM 33-51-00.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,355 hrs · 13,469 cycles
EMERGENCY LIGHT INOPERATIVE. RELAMPED AND OPS CHECKED GOOD IAW AMM 33-51-00.
Part: LIGHT — INTERMITTENT (CABIN) · airframe 19,262 hrs · 13,401 cycles
RT OVERWING EMERGENCY EXIT DOOR LIGHT CYCLES ON AND OFF. PERFORMED OPS CHECK OF RT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (
Part: MEGAPHONE — NO TEST (CABIN) · airframe 19,256 hrs · 13,397 cycles
F/A REPORTS MEGAPHONE DOES NOT TEST PROPERLY. R & R MEGAPHONE IAW AMM 25 61 05, OPS CHECKED GOOD.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 19,104 hrs · 13,295 cycles
EMERGENCY LIGHT INOPERATIVE, LEFT ON ALL NIGHT. RECHARGED EMERGENCY LIGHTS AT GATE, OPS CHECKED NORMAL. DESCREPANCY NO LONGER EXISTS. (SDR CLOSED)
2011
Part: ENGINE — FIRE (LEFT) · airframe 18,274 hrs · 12,715 cycles
WHILE TAXING TO GATE, RECIEVED LEFT ENGINE FIRE WARNING MESSAGE. FIRE WARNING EXTINGUISHED, TAXIED TO GATE. ENGINE WAS ALREADY SHUTDOWN AT TIME OF WARNING. R & R LEFT ENGINE ASSY. ACFT OK FOR SERVICE.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
RT NR 5 SEAT TRACK CORRODED. REPAIRED IAW REO 670-53-00-074, REV A AND EC/TC 670-53-00-074.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
SEAT TRACK CORRODED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-44-AND REO 670-53-00-074.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
LEFT NR 5 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW REO 670-53-00-074, REV A AND EC/TC 670-53-00-074.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
LEFT NR 4 CABIN FLOOR SEAT TRACK CORRODED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49 AND REO 600-53-00-074-054.
Part: ATTACH ANGLE — CRACKED (FAIRING) · airframe 17,472 hrs · 12,163 cycles
THE CENTER ATTACHMENT ASSY FOR FAIRING 194AB HAS A CRACKED NUTPLATE ANGLE. R & R ANGLE WITH NEW IAW SRM 51-42-06.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
FLOOR SUPPORT OF FLOOR PANEL 282GRF HAS CORROSION AROUND NUT PLATES. BLENDED CORROSION AND WAS FOUND TO BE IN LIMITS IAW SRM 53-00-00 AND 51-21-06. MINOR REPAIR.
Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 17,472 hrs · 12,163 cycles
ANGLE THAT FLOORBOARD 141 ALF ATTACHES TO ON FS 280 RIB IS CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-06,51-42-13 & 51-42-21.
Part: FLOOR SUPPORT — CORRODED · airframe 17,472 hrs · 12,163 cycles
CARGO BAY FLOOR SUPPORT FOR PANEL 281HLF HAS CORROSION AROUND NUT PLATES. BLENDED CORROSION AND WAS FOUND TO BE IN LIMITS IAW SRM 53-00-00 AND 51-21-06. MINOR REPAIR.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
SEAT TRACK CORRODED. BLENDED IAW SRM 53-41-49. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW 53-00-49 AND REO 670-53-00-074DSY5003956 6-22-11.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
LEFT AND RIGHT NR1 SEAT TRACK CORRODED AND GOUGED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 53-41-49 AND AMM 53-0-49.
Part: PLACARD — WORN (CABIN) · airframe 17,472 hrs · 12,163 cycles
EXIT PLACARD ON PAX DOOR STEP IS WORN. R & R PLACARD IAW AMM 20-60-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
SEAT TRACK CORRODED. BLENDED CORROSION IAW SRM 52-41-49. MINOR REPAIR.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 17,472 hrs · 12,163 cycles
SEAT TRACK CORRODED. BLENDED SEAT TRACK IAW SRM 51-12-00 AND 53-41-49. MINOR REPAIR.
Part: PLACARD — DAMAGED (EXTERNAL) · airframe 17,472 hrs · 12,163 cycles
ALL EXTERNAL MARKINGS AND PLACARDS ON CREW EMERGENCY ESCAPE HATCH ARE FADED, ILLEGIBLE, MISSING, OR UNREADABLE. R & R PLACARDS IAW AMM 20-60-04.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,472 hrs · 12,163 cycles
FS 280 FLOORBEAM HAS EXFOLIATION CORROSION UPPER SURFACE APPROX LBL 14. R & R DAMAGED FLOORBEAM SECTION WITH NEW IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-24-36, 51-42-02, 51-45-00, 51-42-22.
Part: BULKHEAD — CORRODED (BS 280) · airframe 17,472 hrs · 12,163 cycles
RT 280 BULKHEAD HAS HEAVY CORROSION AFT SIDE JUST ABOVE FLOOR LEVEL AT RBL 12. BLENDED LIGHT SURFACE CORROSION ON BULKHEAD IAW SRM 51-21-06, ORIGINAL MAT'L THICKNESS OF .040, MAT'L LOSS OF .003 NOTED, REMAINING MAT'L THICKNESS OF .037, FOUND TO BE WITHIN LIMITS IAW SRM 53-11-10. MAJOR REPAIR.
Part: VENT — CHAFED (PAX DOOR) · airframe 17,472 hrs · 12,163 cycles
PAX DOOR ICE BREAK CABLE IS CHAFING INTO VENT DOOR. BLENDED CHAFING ON VENT DOOR IAW REO 670-52-11-238. REPAIR AT DAMAGE ON PRESS VENT FLAP ON THE PAX DOOR IS COMPLETED IAW 670-52-11-238 AND MEETS WITH ALL ITS REQUIREMENTS. THIS IS A MAJOR REPAIR. (CLOSED)
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 17,294 hrs · 12,039 cycles
EMERGENCY LIGHTS ARE NOT WORKING. RAN APU AND ARMED EMERGENCY LIGHTS , LIGHTS OPS CHECKED GOOD IAW AMM 33-51-07.
Part: UNKNOWN — ODOR (CABIN) · airframe 16,793 hrs · 11,707 cycles
FA'S REPORT A SLIGHT ODOR THAT INTENSIFIED ON APPROACH AROUND ROWS4 & 5 SIMULAR TO BURNING PLASTIC. OPS CHECKED PACKS. CYCLED THROUGH HIGH/LOW TEMP SETTINGS. COULD NOT DUPLICATE. NO ODORS PRESENT OR DEFECTS NOTED. IAW AMM 21-61-04.
Part: HAND RAIL — OUT OF ADJUST (PAX DOOR) · airframe 16,571 hrs · 11,550 cycles
BOARDING DOOR DIFFICULT TO OPEN. RE-ADJUSTED PAX DOOR HAND RAIL IAW AMM REF 52-11-00. PAX DOOR OPS CKS GOOD AT THIS TIME & DATE. (CLOSED)
2010
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,952 hrs · 10,365 cycles
EMERGENCY EXIT INDENTIFIER HAS 1 EA BULB INOP. REMOVED AND REAPLACED 1EA BULBS AT MAIN PASSENGER CABIN EMERGENCY EXIT IDENTIFIER AT L1 DOOR OPS CHECK GOOD IAW MM 33-51-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,619 hrs · 10,115 cycles
REPLACED AFT CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09. OPS CK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,619 hrs · 10,115 cycles
AFT CEILING EMERGENCY FLOOD LIGHT INOP.
Part: LIGHT — INOPERATIVE (EXTERNAL EMERG) · airframe 14,130 hrs · 9,764 cycles
RT REAR EXTERNAL EMERGENCY LIGHT INOP. R & R RT REAR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD.
2009
Part: PLACARD — MISSING (PAX DOOR) · airframe 13,843 hrs · 9,548 cycles
PAX DOOR EXIT PLACARD MISSING. FLT 5592 DEL 53 MINS.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,420 hrs · 9,213 cycles
LT OVERWING EMERGENCY EXIT LWR EMERGENCY LIGHT HAS SEVERAL INOP BULBS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,466 hrs · 8,483 cycles
EMERGENCY LIGHTS DO NOT OPERATE WHEN TURNED ON WITH EITHER THE COCKPIT OR THE FLIGHT ATTENDANT PANEL SWITCH.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 11,857 hrs · 7,996 cycles
RT VERTICAL STABILIZER DRAG ANGLE VERIFIED CRACKED. REPAIRED PER REO 670-55-31-041.
Part: WEB — CRACKED (FUSELAGE) · airframe 11,857 hrs · 7,996 cycles
RT 280 WEB P/N CC670-34117-6 FOUND CRACK.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,857 hrs · 7,996 cycles
FWD FLOORBEAM ANGLE AT FS 280 IS CORRODED. REMOVED FWD SUPPORT FLOOR ANGLE IAW SRM 51-42-06 AND 51-42-20. DRILLED AND INSTALLED NEW FWD SUPPORT FLOOR ANGLE PER SRM 51-40-11 AND 51-42-06. BAT7023167. RII C/W SATISFACTORY IAW SP 607 & SRM 51-40-11.
Part: BULKHEAD — CORRODED (BS 280) · airframe 11,857 hrs · 7,996 cycles
RIGHT FS 280 BULKHEAD LOWER WEB HAS SURFACE CORROSION. BLENDED RT WEB TO WITHIN LIMITS CONDITION IAW SRM 53-11-10.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,857 hrs · 7,996 cycles
FS 280.00 LT CROSS BEAM CORRODED ON TOP FLANGE. REMOVED AND REPLACED 280 LT CROSSBEAM PER SRM 51-40-11 AND 51-42-00.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,857 hrs · 7,996 cycles
FS 280.00 RT CROSS BEAM CORRODED ON TOP FLANGE. REMOVE AND REPLACED RT CROSSBEAM PER SRM 51-40-11 AND 51-42-00.
Part: WEB — CORRODED (BS 280) · airframe 11,857 hrs · 7,996 cycles
LT SIDE FS 280.00 WEB ABOVE FLOOR CORRODED LOWER RT EDGE. REMOVED WEB IAW SRM 51-42-06, DRILLED NEW WEB IAW SRM 53-11-10, INSTALLED WEB PER SRM 51-42-06.
Part: SHROUD — CRACKED (SPOILERS) · airframe 11,856 hrs · 7,996 cycles
RT MULTIFUNCTION SPOILER SHROUD CRACKED AT I/B CORNER. REMOVED PAINT, RE-INSPECTED AND FOUND RT MULTIFUNCTION SPOILER SHROUD NOT CRACKED AT I/B CORNER. PRIMED AND PAINTED PER SRM 51-21-16 02-16-09.
Part: DRAG ANGLE — CRACKED (AIRSTAIR DOOR) · airframe 11,857 hrs · 7,996 cycles
ASD AFT SIDEWALL DRAG ANGLE CRACKED.
Part: STEP — BROKEN (PAX DOOR) · airframe 11,857 hrs · 7,996 cycles
PAX DOOR BOTTOM STEP BROKEN AT LINK ATTACK POINT. REMOVED AND REPLACED BROKEN STAIR PANEL IAW CMM 52-11-00. REMOVED AND REPLACED BROKEN STAIR PANEL IAW CMM 52-11-00.
Part: STEP — CRACKED (AIRSTAIR) · airframe 11,857 hrs · 7,996 cycles
ASD TOP STEP CRACKED. INSTALLED NEW TOP STEP IAW AMM 52-11-04. OPERATIONAL CHECK COMPLIED WITH IAW AMM 52-11-04-710-801. RII COMPLIED WITH IAW S.P. 607 AND AMM 52-11-04.
Part: LIGHT — FAILED (CABIN) · airframe 11,737 hrs · 7,908 cycles
DURING ORG CHECK EMERGENCY LIGHT TEST FAILED. NO EMERGENCY LIGHT STATUS MSG OR CABIN EMERGENCY LIGHTING WITH SWITCH IN ON POS...FLT 5189 CX.
2008
Part: SIGN — INOPERATIVE (CABIN) · airframe 10,586 hrs · 7,052 cycles
LT OVERWING EMERGENCY EXIT LOWER LIGHTED EXIT SIGN HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED LT LOWER EMERGENCY EXIT SIGN BAD BULBS IAW CRJ 700 AMM 33-51-05. (S)
2007
Part: STEP — DAMAGED (AIR STAIR) · airframe 8,881 hrs · 5,843 cycles
ASD LOWER STEP DAMAGED.
Part: FLASHLIGHT — DISCHARGED (CABIN) · airframe 8,444 hrs · 5,555 cycles
FWD F/A FLASHLIGHT WEAK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,222 hrs · 5,412 cycles
FWD EMERGENCY LIGHT ABOVE ROW TWO IS INOP, CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS.
Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 7,869 hrs · 5,182 cycles
FIRE SYS FAULT, STATUS MSG. COMES ON & OFF THROUGHOUT FLIGHT.
Part: PANEL — CORRODED (T/E FLAP) · airframe 7,541 hrs · 4,956 cycles
FOUND EXFOLIATION CORROSION ON INTERNAL STRUCTURE OF LT OUTBOARD FLAP ASSY IAW TASKCARD 000-57-590-502. REMOVED AND REPLACED LT OUTBOARD FLAP PANEL IAW CRJ 700 AMM 27-52-29. RIG AND OP'S CHECK GOOD IAW CRJ 700 AMM 27-52-00. STARTED REMOVING FLAP FAIRING PANEL BRACKETS FROM OLD FLAP ASSY AND REINSTALLING ON NEW LT FLAP ASSY AS REQUIRED PER CRJ 700 SRM 51-42-00. COMPLETED REMOVAL AND TRANSFER OF FLAP FAIRING BRACKETS IAW CRJ 700 SRM 51-42-00. 06/27/2007 JOB COMPLETE. C/W RII IAW SP 607 AND CRJ 700 AMM 27-52-00. SUPPLEMENTAL - SDR CLOSED 06/29/07.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,541 hrs · 4,956 cycles
LT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW SRM 51-42-06, 70-53-11-052, REO 670-53-11-052, ALL WORK COMPLETE COMPLIED WITH EO 700-53-0062 01
Part: BULKHEAD — CORRODED (BS 280) · airframe 7,541 hrs · 4,956 cycles
RT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW CRJ700 SRM 51-42-06, REO 670-53-11-052, SRM 51-00-00, AND EO 700-53-0062.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,541 hrs · 4,956 cycles
LT 280 CROSSBEAM CORRODED AND CRACKED. REPAIRED IAW CRJ700 SRM 51-42-21, CRJ700 SRM 51-42-06, CRJ 700 SRM 51-42-00, REO 670-53-11-00026, & REO 670-53-11-047.
Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 7,541 hrs · 4,956 cycles
RT SEAT TRACK CORRODED BETWEEN FS349-364. REPAIRED IAW SRM`S 53-21-49 AND 51-21-06, AND 51-41-02.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,541 hrs · 4,956 cycles
FLIGHT COMPARTMENT FLOORBOARD AFT LANDING BRACKET CRACKED AT FS 280.00. [06-27-07] REPAIRED IAW 51-00-00, 51-00-00, AND REO 670-53-11-047.
Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 7,541 hrs · 4,956 cycles
RIGHT EMERGENCY EXIT DOOR UPPER HANDLE COVER IS CRACKED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 7,541 hrs · 4,956 cycles
FS 280.00 INTERCOSTAL BETWEEN LBL 9 AND RBL 9 CORRODED ON FWD FACE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,085 hrs · 4,629 cycles
RIGHT EMERGENCY EXIT LOWER EXIT LIGHT HAS SEVERAL INOP BULBS.
2006
Part: PANEL — CRACKED (FUSELAGE)
DURING A C-CHECK, THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, IAW REO 670-52-11-104. (K)
Part: STEP — SEPARATED (PAX DOOR)
DURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND SEPARATED AT THE ATTACH STAY ROD BRACKET TO THE STEP COMPOSITE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2004
Part: VANE — FALSE INDICATION (AOA)
FOLLOWING TAKEOFF, CREW RECEIVED A STALL FAIL CAUTION MESSAGE. QRH WAS COMPLIED WITH AND APPROXIMATELY 250 KNOTS THE STICK SHAKER BEGAN TO SHAKE THE CONTROLS. THE AIRSPEED WAS INCREASED ABOVE 250 KNOTS AND PITCH LOWERED TO INCREASE ABOVE THE LOW SPEED CUE. UPON LOWERING THE PITCH AND INCREASING AIRCRAFT SPEED, THE SPEED CUE CONTINUED TO CLIMB, BEING UNABLE TO STOP THE STICK SHAKER. EMERGENCY WAS DECLARED WITH THE AIRCRAFT RETURNING, LANDING SAFELY. MAINTENANCE FOUND THE LEFT ANGLE OF ATTACK VANE (TRANSDUCER) COVERED WITH A PLASTIC BAG PREVENTING IT FROM MOVING. MAINTENANCE REMOVED AND REPLACED THE LT ANGLE-OF-ATTACK (AOA) VANE IAW VANE IAW AMM 27-35-05. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.