N723EV
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.
249 reports on file, 2004-03-08 – 2025-04-16.
Part: FRAME — CORRODED (ZONE 100) · 24,946 cycles
FRAME FS 1051.30 CORRODED BETWEEN STGR 27 AND STGR 25LH #29987334 (C-CHECK RO 07/18/2025)REPAIRED FRAME AT FS1051.30 BETWEEN STGR 27 AND STGR 25LH IAW REO 670-53-61-2500 REV -- 2025-05-26. COMPLIED WITH ALL STEPS OF REO 670-53-61-2500 REV -- 2025-05-26. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: WINDOW POST — DAMAGED (ZONE 200) · 24,946 cycles
RIGHT WINDSHIELD POST FITTING PN: GC212-0046-4, WHEN REMOVED FOUND FASTENERS HOLES PREVIOUSLY COUNTER SUNK, BUT REQUIRE PROTRUDING HEAD FASTENERS NOT FLUSH FASTENERS. REPLACE PARTS. REPLACED RH WINDSHIELD POST FITTING PN: GC212-0046-4 WITH NEW IAW SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV. F. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: SUPPORT ANGLE — CORRODED (ZONE 800) · 24,946 cycles
(MX 29814919) CORROSION NOTED ON PAX DOOR FWD ANGLE SUPPORT. (C-CHECK RO 07/18/2025) INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT P/N 601R318731-3. IAW. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: INTERCOSTAL — CORRODED (ZONE 800) · 24,946 cycles
(MX 29815563) CORROSION NOTED ON INTERCOSTAL FWD DD3 CLIP (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR INTERCOSTAL FWD DD3 CLIP REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DETAILS.
Part: FRAME — CORRODED (ZONE 200) · 24,946 cycles
CORROSION FOUND ON INBOARD UPPER FLANGE OF RBL9 AT FS 549. PERFORMED FLANGE REPAIR ON INBOARD UPPER FLANGE OF RBL9 AT FS 549 INSTALLED ANGLE (18) , FILLER (23) AND SHIM (19) REF CRJ700 SRM 53-00-41-201-001-A01AND COMPLIED WITH ALL THE STEPS OF THE REO 670-53-31-1018 REV --, COMPLIEDWITH 51-900-1002-SKY
Part: CLEAT — CORRODED (ZONE 800) · 24,946 cycles
(MX 29809807) CORROSION NOTED ON PAX DOOR CLEAT OF FORMER FS329.41 AND DD6 INTERCOSTAL (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR CLEAT OF FORMER FS329.41 AND DD6 INTERCOSTAL. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · 24,946 cycles
CORROSION FOUND ON RBL9 FLOOR BEAM BETWEEN FS847 AND FS863. (C-CHECK RO 07/18/2025)REMOVED AND REPLACED RBL9 FLOOR BEAM BETWEEN FS847 AND FS863 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-35920 REV. M ALL CHECKS GOOD SEE CONTINUATION TASKS FOR MORE DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: INTERCOSTAL — CORRODED (ZONE 200) · 24,946 cycles
( MX 29796801) CORROSION NOTED ON INTERCOSTAL FWD DD7 CLIP (C-CHECK RO 07/18/2025)INSTALLED NEW INTERCOSTAL FWD DD7 CLIP. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: INTERCOSTAL — CORRODED (ZONE 200) · 24,946 cycles
( MX 29796784) CORROSION NOTED ON INTERCOSTAL FWD DD1 CLIP (C-CHECK RO 07/18/2025)INSTALLED NEW INTERCOSTAL FWD DD1 CLIP. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: INTERCOSTAL — CORRODED (ZONE 800) · 24,946 cycles
(MX 29789703) CORROSION NOTED AT PAX DOOR FWD INTERCOSTAL DD3 (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 800) · 24,946 cycles
(MX 29789709) CORROSION NOTED AT PAX DOOR FWD INTERCOSTAL DD2 (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD2. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: ANGLE — CORRODED (ZONE 800) · 24,946 cycles
(MX 29789718) CORROSION NOTED AT PAX DOOR ANGLE BETWEEN FORMER FS. 327.963 AND FRAME FS. 327.763 LINE DD7A. (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR ANGLE P/N 601R317052-1, BETWEEN FORMER FS. 327.763 AND FRAME FS. 338.963 LINE DD7A. IAW. CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01. DWG 601R317052 REV. B AND DWG 601R31702 REV. N, LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: FLOORBEAM — CORRODED (ZONE 200) · 24,946 cycles
CORROSION FOUND ON INBOARD UPPER FLANGE ON FLOORBEAM LBL 9 AT FS 549 (C-CHECK RO 07/18/2025)COMPLIED WITH ALL STEPS OF REO 670-53-31-1022 REV-- DATE 2025-04-02, AND REO 670-53-31-1020 REV -- 2025-04-14 IN THE REPAIR ON INBD UPPER FLANGE ON FLOORBEAM LBL9 AT FS549. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKY
Part: FORMER — CORRODED (ZONE 800) · 24,946 cycles
(MX 29789716) PAX DOOR FORMER F/S 311.75 IS CORRODED AT DD1 AND DD6 LOCATION (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR AFT FORMER FS. 311.75 AT DD1 AND DD6 LOCATION IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. AND DWG 601R31702 REV.N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DETAILS.
Part: INTERCOSTAL — CRACKED (ZONE 800) · 24,946 cycles
PAX DOOR SUSSPECTED CRACK ON AFT DD7 INTERCOSTAL. INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7. IAW SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: STRINGER — CORRODED (ZONE 100) · 24,946 cycles
STRINGER 24R HAS CORROSION BETWEEN FS295 - FS310 (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW AVIONICS BAY STRINGER 24R BETWEEN FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: STRINGER — DAMAGED (ZONE 100) · 24,946 cycles
UPON REMOVAL OF PREVIOUS REPAIR DOUBLER AT FS293 - FS312 BETWEEN 2" ABOVE STR 24R AND 2" BELOW STR 25R FOR ACCESS TO REPLACE STRINGER 25R (CAMP 29634791 JOB HN00220902) FOUND UNDERLYING SKIN DAMAGE (C-CHECK RO 07/18/2025)REPAIRED DAMAGED SKIN AT FS293 - FS312 2" ABOVE STR 24R AND 2" BELOW STR 25R REF CRJ-700 SRM 51-42-21-001-001-A01 AND REO 670-53-21-2582 REV -- DATE 2025-03-12. COMPLIED WITH ALL STEPS OF REO 670-53-21-2582 REV -- DATE 2025-03-12. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: FITTING — CRACKED (ZONE 400) · 24,946 cycles
LEFT PYLON SS DOUBLER HAS MULTIPLE CRACKS RADIATING FROM AROUND THE FITTING FOR THE ENGINE DRIVEN PUMP PRESSURE LINE, UNDER PANEL 412BB, 412BT & 412CT. (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED DOUBLER ON PYLON FIREWALL WEB WITH NEW P/N MM670-37001-989 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG MM670-37001 REV AH. LEAK CHECKS GOOD, OPS TEST GOOD, OIL CONSUMPTION GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: WEB — CRACKED (ZONE 400) · 24,946 cycles
LEFT PYLON SS WEB HAS MULTIPLE CRACKS RADIATING FROM AROUND THE FITTING FOR THE ENGINE DRIVEN PUMP PRESSURE LINE, UNDER PANEL 281AZ. (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW FIREWALL WEB ON LH ENGINE PYLON BETWEEN FS 1069 AND FS 1088 PER REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-41-02-001-001-A01 AND DWG# MM670-37001 REV AH. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: WEB — CRACKED (ZONE 100) · 24,946 cycles
PREVIOUS REPAIR OF THE TRU BAY FLOOR SKIN AT THE ADG HYD PUMP HAS A CRACK IN THE RADIUS AROUND THE FS192.5 FRAME. (MARKED) (C-CHECK RO 07/18/2025)PERFORMED REPAIR OF TRU BAY DOOR FLOOR SKIN AT FS 193 RHS PER REO 670-53-11-509 REV E DATED 2018-02-08 ALL STEPS COMPLIED WITH.. OPS TEST GOOD. COMPLIED WITH 51-900-1002-SKY
Part: ATTACH ANGLE — CORRODED · 24,946 cycles
SURFACE CORROSION ON LEFT REAR SPAR ATTACH ANGLE FOR TIRE BURST PANEL 542AZ (C-CHECK RO 07/18/2025)REPLACED LEFT REAR SPAR ATTACH ANGLE FOR TIRE BURST PANEL 542AZ REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG # CC670-10320 REV : F. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
Part: STRINGER — CORRODED (ZONE 100) · 24,946 cycles
AVIONICS BAY STRINGER 26L BETWEEN FS280- FS295 IS CORRODED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW STRINGER 26L FROM FS280- FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: STRINGER — CORRODED (ZONE 100) · 24,946 cycles
AVIONICS BAY STRINGER 23R BETWEEN FS310 - FS319 IS CORRODED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW AVIONICS BAY STRINGER 23R BETWEEN FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG SH670-31630 REV K AND REO 670-53-21-2581 REV -- DATE 2025-03-03. COMPLIED WITH ALL STEPS OF REO 670-53-21-2581 REV -- DATE 2025-03-03. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: STRINGER CLIP — CORRODED (ZONE 100) · 24,946 cycles
STRINGER CLEAT AT 21R FS333 IS CORRODED (MX 29635322) (C-CHECK RO 07/18/2025)INSTALLED NEW STRINGER CEAT 21R AT FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-32600 REV AK. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: WINDOW POST — CRACKED (ZONE 200) · 24,946 cycles
R/H WINDSHIELD POST IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW RH WINDSHIELD POST REF CRJ 700SRM 51-42-21-001-001-A01, DWG. CC670-33055 REV. F, AND REO 670-53-11-2126 REV. A. DATE: 2025-04-25. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: STRINGER — CORRODED (ZONE 100) · 24,946 cycles
STRIGER 25R IS CORRODED BETWEEN F/S 280 AND F/S 295 (MX 29634791) (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW STRINGER 25R FROM FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: FRAME — CORRODED (ZONE 100) · 24,946 cycles
FRAME F/S 319 IS CORRODED AT STRG 27 (MX 29634776) (C-CHECK RO 07/18/2025)INSTALLED NEW LOWER FRAME SECTION FS319 BETWEEN STR 23R - STR 21L REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV KCOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, LEAK CHECK GOOD
Part: INTERCOSTAL — CORRODED (ZONE 800) · 24,946 cycles
CORROSION NOTED ON PAX DOOR INTERCOSTAL MID DD6 (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR INTERCOSTAL MID DD6 REF CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DETAILS.
Part: CLEAT — CORRODED (ZONE 100) · 24,946 cycles
STRINGER CLEAT AT 23R FS319 IS CORRODED (C-CHECK RO 07/18/2025)STRINGER CLEAT AT 23R FS319 IS FOUND TO BE OUT OF LIMITS 100% MATERIAL LOSS REFCRJ-700 SRM 53-21-03-101-002-A01REMOVED AND REPLACED STRINGER CLEAT P/N SH670-35625-1 AT 23R FS319 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31630 REV K, COMPLIED WITH 51-900-1002-SKY
Part: HINGE — GOUGED (ZONE 200) · 24,946 cycles
PAX DOOR HINGE ( FUSELAGE SIDE ) AFT MOST LUG LAND IS GOUGED. HN00219949 (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE ON THE FUSELAGE SIDE REF CRJ 700 SRM 53-21-23-201-007-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND DWG SH670-31810 REV. AE. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: HINGE — GOUGED (ZONE 200) · 24,946 cycles
PASSENGER DOOR PIANO HINGE LUG NUMBER 1 AND 7 GOUGED (FROM FORWARD SIDE OF DOOR) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PASSENGER DOOR PIANO HINGE REF. CRJ700 SRM 52-11-01-201-002-A01, CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DRW 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DETAILS. REPLACED PART NO WEIGHT CHANGE.
Part: SKIN — SCRATCHED (ZONE 100) · 24,946 cycles
FORWARD DRAIN MAST EXTERIOR SKIN PENETRATION FORWARD INBOARD FASTENER HOLE HAS MULTIPLE SCRATCHES AFT OF FS333.00 BETWEEN STGR25R - STGR24R (C-CHECK RO 07/18/2025)COMPLIED WITH REO 670-53-21-2588 REV -- DATED 2025-03-12 REPAIR FORWARD DRAIN MAST EXTERIOR SKIN FASTENER HOLE SCRATCHES AFT OF FS333.00 BETWEEN STGR25R - STGR24R COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)INSTALLED NEW R/H UPPER TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED CRACKED INBD "A" STANDOFF FROM L/H LOWER TRANSCOWL AND INSTALLED 1 EA NEW INBD STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF GREO #670-54-21-971 REV (-B) 2023-11-28 STEPS 1-3. COMPLIED WITH FORM M-337 FOR A MAJOR REPAIR AND SKY CARD #51-900-1002-SKY.
Part: CHANNEL — CORRODED (ZONE 100) · 24,946 cycles
CORROSION ON AFT WATER DRAIN MAST CHANNEL (C-CHECK RO 07/18/2025)INSTALLED AFT DRAIN MAST CHANNEL REF SRM 51-42-06-001-001-A01,DWG:MM670-43200 REV NC. PRESSURE CHECK AND OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: STIFFENER — SHEARED (ZONE 400) · 24,946 cycles
R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 07/18/2025)ON R/H LOWER TRANSCOWL, 3 EA. FASTENER HOLES COMMON TO ZED STIFFENER P/N CN624-2038-203 ON INNER SKIN FOUND TO BE CRACK FREE WITH NO DAMAGE NOTED. ENGINEERING REQUIRED FOR ALTERNATE METHOD OF FASTENER INSTALLATION IN FROM OUTER SKIN DO TO ACCESS, REF. REO 670-54-21-1714, REV. --, 2025-02-12. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY, CAMP 29586797.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER 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. CAMP 29587231.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER 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. CAMP 29587221.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER 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. CAMP 29587221.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED CRACKED OUTBD "A" STANDOFF FROM L/H LOWER TRANSCOWL AND INSTALLED 1 EA NEW OUTBD STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF GREO #670-54-21-971 REV (-B) 2023-11-28 STEPS 1-3. COMPLIED WITH FORM M-337 FOR A MAJOR REPAIR AND SKY CARD #51-900-1002-SKY.
Part: STAND OFF — CRACKED (ZONE 400) · 24,946 cycles
R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER 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. CAMP 29587073.
Part: SKIN — DEBONDED (ZONE 500 AILERON) · 24,946 cycles
LH AILERON OUTBD EDGE CORNER. DISBONDED. (C-CHECK RO 07/18/2025)REMOVED AND REPLACED RUBBING BLOCK PN: CC670-13076-3 REF. CRJ 700 SRM 51-42-13-001-001-A01, INSTALLED NEW LH AILERON O/B RIB REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DRWG CC670-13000 REV. D AND REO 670-57-61-441 REV. -- DATED 2025-04-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: SKIN — CORRODED (ZONE 100) · 24,946 cycles
CORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R AS MARKED (C-CHECK RO 07/18/2025)REPAIRED CORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R IAW REO 670-53-21-2585 REV -- DATED 2025-03-18. COMPLIED WITH ALL STEPS OF REO 670-53-21-2585 REV -- DATED 2025-03-18. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED. PERFORMED PRESSURE LEAK CHECK REF CRJ 700 SRM 51-23-03-001-001-A01. NO LEAKS NOTED AT THIS TIME.
Part: FRAME — CORRODED (ZONE 100) · 24,946 cycles
CORROSION ON FS 310.0 FORWARD FLANGE BETWEEN STGR27 AND STGR26R AS MARKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED WITH NEW LOWER FRAME SECTION P/N SH670-31354-3 AND FRAME SPLICES AT FS310 FROM STR 25R TO STR 25L REF CRJ-700 SRM 53-00-06-201-006-A01 COMPLIED WITH 51-900-1002-SKYPERFORMED PRESSURE LEAK CHECK, NO LEAKS NOTED AT THIS TIME
Part: STRINGER — CORRODED (ZONE 100) · 24,946 cycles
CORROSION ON STGR25R BETWEEN FS 319.7 AND FS333.0 AS MARKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED WITH NEW STRINGER SPLICE P/N SH670-32429-4 AT STR 25R FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV EPERFORMED PRESSURE LEAK CHECKREF CRJ 700 SRM 51-23-03-001-001-A01. NO LEAKS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DOOR SILL — CHAFED (ZONE 100) · 24,946 cycles
DURING AUDIT OF 1C TASK CARD 53-280-507 (DETAILED INSPECTION OF THE EXTERNAL FACE OF THE SILL, EDGE FRAMES, AND DOOR FITTINGS AROUND THE AFT BAGGAGE-BAY DOOR CUTOUT EXCEPT THE AREA UNDER THE PROTECTOR PLATE), FOUND CHAFFING ON THE LOWER FWD EDGE FRAME OF AFT CARGO DOOR CUTOUT AND NEEDS SPOT PAINT. (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW LOWER AFT CARGO DOOR COAMING REF CRJ700 SRM 51-41-02-001-001-A01. PERFORMED PRESSURE LEAK IAW CRJ 700 AMM 21-31-00-910-801-A01. LEAK CHECK GOOD. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: FITTING — CRUSHED (ZONE 800) · 24,946 cycles
AFT BAGGAGE-BAY DOOR, AFT CROTCH FITTING SMASHED, INBOARD SIDE OF FITTING, HN00218513 (C-CHECK RO 07/18/2025)COMPLIED WITH REO 670-53-61-2481 REV --, DATED 2025-03-19 STEPS 1-7. REF CRJ700 SRM 51-12-00-001-001-A01 REV.38 DATED JUL/25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CARD FOR DETAILS.
Part: STOP — WORN (ZONE 800) · 24,946 cycles
AFT BAGGAGE-BAY DOOR, FORWARD LOWER STOP FITTING WORN, HN00218516 (C-CHECK RO 07/18/2025)REMOVED DAMAGE ON AFT BAGGAGE-BAY DOOR, FORWARD LOWER STOP FITTING. REF CRJ700 SRM 51-12-00-001-001-A01. AND REPAIRED PER REO 670-53-61-2481 REV --, DATED 2025-03-19. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FITTING — CRUSHED (ZONE 800) · 24,946 cycles
AFT BAGGAGE-BAY DOOR, FORWARD CROTCH FITTING SMASHED, INBOARD SIDE OF FITTING, HN00218512 (C-CHECK RO 07/18/2025)REMOVED DAMAGE ON AFT BAGGAGE-BAY DOOR, FORWARD CROTCH FITTING, INBOARD SIDE OF FITTING. REF CRJ700 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIR PER REO 670-53-61-2481 REV --, DATED 2025-03-19 ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · 24,946 cycles
FUSELAGE FLOOR SILL, RIGHT FS693 TO FS708, CORROSION AROUND FASTNER HOLES, REPAIRED RH FUSELAGE FLOOR SILL FROM FS693 TO FS708 REF REO 670-53-41-725 REV A, AND SRM 51-21-06-001001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHECK GOOD.
Part: ROLLER — OUT OF LIMITS (ZONE 500 SLAT) · 24,946 cycles
L/H WING SLAT TRACK 2-2 UPPER TRACK ROLLER HAS FLAT SPOTS OUT OF LIMITS (C-CHECK RO 07/18/2025)REMOVED L/H WING SLAT TRACK 2-2 TOP AFT ROLLER AND INSTALLED NEW SERVICABLE ROLLER. GAP CHECK GOOD. ELECTRICAL EXTENSION AND RETRACTION OF FLAPS AND SLATS ACCOMPLISHED, SYSTEM CHECKS GOOD AT THIS TIME.
Part: ROLLER — OUT OF LIMITS (ZONE 500 SLAT) · 24,946 cycles
L/H WING SLAT TRACK 1-2 INBOARD UPPER ROLLER HAS FLAT SPOT OUT OF LIMITS (C-CHECK RO 07/18/2025)REMOVED L/H WING SLAT TRACK 1-2 INBOARD AFT ROLLER AND INSTALLED NEW SERVICABLE ROLLER. GAP CHECK GOOD. ELECTRICAL EXTENSION AND RETRACTION OF FLAPS AND SLATS ACCOMPLISHED, SYSTEM CHECKS GOOD AT THIS TIME.
Part: ROLLER — WORN (ZONE 500 SLAT) · 24,946 cycles
L/H WING SLAT TRACK 3-2 INBOARD AND OUTBOARD SIDE ROLLERS HAVE WEAR MARKS AND DO NOT SPIN FREELY (C-CHECK RO 07/18/2025)REMOVED L/H WING SLAT TRACK 3-2 OUTBOARD AND INBOARD FWD & AFT SIDE ROLLERS AND INSTALLED NEW SERVICABLE ROLLERS ON L/H WING SLAT TRACK 3-2 OUTBOARD AND INBOARD FWD & AFT SIDES. ELECTRICAL RETRACTION AND GAP CHECKS GOOD AT THIS TIME.
Part: ROLLER — OUT OF LIMITS (ZONE 500 SLAT) · 24,946 cycles
L/H WING SLAT TRACK 2-2 OUTBOARD UPPER ROLLER HAS FLAT SPOTS OUT OF LIMITS (C-CHECK RO 07/18/2025)REMOVED L/H WING SLAT TRACK 2-2 OUTBOARD AFT SIDE ROLLER AND INSTALLED NEW SERVICABLE ROLLER. GAP CHECK GOOD. ELECTRICAL EXTENSION AND RETRACTION OF FLAPS AND SLATS ACCOMPLISHED, SYSTEM CHECKS GOOD AT THIS TIME.
Part: ROLLER — DAMAGED (ZONE 500 SLAT) · 24,946 cycles
L/H WING SLAT TRACK 2-2 INBOARD LOWER ROLLER DOES NOT MOVE FREELY (C-CHECK RO 07/18/2025)REMOVED L/H WING SLAT TRACK 2-2 INBOARD FWD SIDE ROLLER AND INSTALLED NEW SERVICABLE ROLLER. GAP CHECK GOOD. ELECTRICAL EXTENSION AND RETRACTION OF FLAPS AND SLATS ACCOMPLISHED, SYSTEM CHECKS GOOD AT THIS TIME.
Part: SLAT TRACK — OUT OF LIMITS (ZONE 600) · 24,946 cycles
R/H WING SLAT TRACK 3-2 OUTBOARD LOWER ROLLER HAS FLAT SPOTS OUT OF LIMITS (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW SERVICABLE R/H WING SLAT TRACK 3-2 OUTBOARD FWD SIDE ROLLER REF. CRJ-700 AMM 27-81-44-400-803-A01 TORQUE WRENCH TUC6232 CAL DUE: 31-OCT-2025 GAP CHECK GOOD.
Part: ROLLER — OUT OF LIMITS (ZONE 600 SLAT) · 24,946 cycles
R/H WING SLAT TRACK 1-2 INBOARD UPPER ROLLER HAS FLAT SPOTS OUT OF LIMITS (C-CHECK RO 07/18/2025)REMOVED RH WING SLAT TRACK 1-2 INBOARD UPPER ROLLER AND REPLACED WITH SERVICEABLE ROLLER FROM STOCK. REF CRJ 700 AMM 27--81-44-400-801-A01 ELECTRICAL RETRACTION ANG GAP CHECKS GOOD AT THIS TIME.
Part: SHAFT — DENTED (ZONE 500 FLAP) · 24,946 cycles
LEFT INBOARD FLAP, SECOND FROM RIGHT VANE ACTUATOR SHAFT HAS INDENT, HN00217959 (C-CHECK RO 07/18/2025)REPAIRED LEFT INBOARD FLAP, SECOND FROM RIGHT VANE ACTUATOR SHAFT INDENT REF REO 670-57-52-257 REV -A DATED 2024-08-20 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY OPS CHECK GOOD
Part: STRIKER — CORRODED (ZONE 800) · 24,946 cycles
DURING AUDIT OF 1C TASK CARD 53-230-504(DETAILED INSPECTION OF THE GALLEY SERVICE DOOR (FORWARD) EXTERNALSURROUND STRUCTURE AND FITTINGS - FS319.70 TO FS349.00, STGR9R TOSTGR18R (EES)) FOUND POSSIBLE CORROSION THE LOWER INBOARD SIDE OF THE SVC DR SEAL STRIKER. (C-CHECK RO 07/18/2025)REMOVED AND REPLACED SEAL STRIKER P/N SH670-31412-3 REF SRM 51-42-06-001-001-A01 & DWG SH670-31950 REV YPERFORMED PRESSURE CHECK OF SERVICE DOOR SEAL AND STRIKER REF AMM 21-31-00-910-801-A01. NO LEAKS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SKIN — GOUGED (ZONE 100) · 24,946 cycles
FORWARD CARGO DOOR SURROUND STRUCTURE -FORWARD EDGE OF THE DOOR OPENING THE SKIN IS GOUGED BELOW THE TWO FORWARD GUIDE FITTINGS APPX FS535.00. (MARKED) (C-CHECK RO 07/18/2025)ORIGINAL MATERIAL THICKNESS IS 0.160", MINIMUM REMAINING THICKNESS IS 0.139" FOR A MATERIAL LOSS OF 0.021" REF DWG SH670-34126 REV C. FOUND TO BE OUT OF ALLOWABLE LIMITS OF MAX 10% MATERIAL LOSS REF CRJ700 SRM 53-31-23-101-001-A01REMOVED AND REPLACED SEAL STRIKER WITH NEW P/N SH670-34126-8 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-33750 REV AAPERFORMED PRESSURE LEAK CHECK APPROX. FS535.00 , REF CRJ 700 AMM 52-00-00-790-801-A01. NO LEAKS NOTED AT THIS TIME.
Part: INTERCOSTAL — CORRODED (ZONE 100) · 24,946 cycles
BELOW FLOOR INTERCOSTAL AT STR.20R BETWEEN FS.319.70 AND FS.333.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 07/18/2025)REMOVED AND REPLACED INTERCOSTAL AT STR.20R BETWEEN FS.319.70 AND FS.333.00 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-32004 REV A, COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION TASKS FOR MORE DETAILS.
Part: REPAIR — GOUGED (ZONE 100) · 24,946 cycles
THE DOUBLER REPAIR ON THE EXTERIOR JUST AFT OF FS977 BETWEEN STR26L AND STR26R HAS MULTIPLE GOUGES (C-CHECK RO 07/18/2025) REMOVED DAMAGED DOUBLER AND INSTALLED REPAIR PARTS. REF REO# 670-53-00-290 REV:-F DATE: 2019/04/26. LEAK CHECK GOOD . COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DRAG ANGLE — CRACKED (ZONE 300) · 24,946 cycles
VERTICAL STAB. LH AFT DRAG ANGLE HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 07/18/2025)REPAIRED VERTICAL STAB LH AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01 REPAIR. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · 24,946 cycles
RH TRU DOOR SILL SUPPORT ANGLE HAS SUSPECTED CRACK ON AFT LATCH CUT OUT (MARKED). (C-CHECK RO 07/18/2025)REMOVED CRACKED AND INSTALLED NEW RH TRU DOOR SILL SUPPORT ANGLE REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, DWG# CC670-33040 REV G AND REO 670-53-11-2118 REV-- DATE:2025-03-28. SEE CONTINUATION CARD FOR DETAILS, COMPLIED WITH 51-900-1002-SKY
Part: DRAG ANGLE — CRACKED (ZONE 300) · 24,946 cycles
VERTICAL STAB. RH AFT DRAG ANGLE HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 07/18/2025)REPAIRED VERTICAL STAB RH AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01 REPAIR COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: SKIN — GOUGED (ZONE 800) · 24,946 cycles
PASSENGER DOOR EXTERNAL SKIN IS GOUGED ALONG THE FORWARD HALF OF THE TOP EDGE OF THE DOOR. REPAIRED PASSENGER DOOR EXTERNAL SKIN FORWARD HALF OF THE TOP EDGE OF THE DOOR.ALL STEPS COMPLIED WITH IAW REO 690-52-11-1017 REV. -- DATED 2025-03-04. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: SKIN — DENTED (ZONE 100) · 24,946 cycles
EVALUATE DENT ON EXTERNAL FUSELAGE SKIN AT FS 409.00 BETWEEN STGR 21R - 22R (C-CHECK RO 07/18/2025)EVALUATED DENT, AFTER A VISUAL INSPECTION, 1 LIGHTING STRIKE WAS FOUND. REPAIRED LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN AT FS 409.00 BETWEEN STGR 21R - 22R IAW CRJ 700 SRM 53-00-00-201-003-A01. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: SKIN — DENTED (ZONE 100) · 24,946 cycles
EVALUATE PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 295.00 - 310.00, STGR 25L - 26L (C-CHECK RO 07/18/2025)REPAIRED PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 295.00 - 310.00, STGR 25L - 26L REF REO 670-53-21-2591 REV -- DATED 2025-03-22 AND REO 670-51-00-085 REV -A DATED 2017-08-23
Part: SKIN — DAMAGED (ZONE 100) · 24,946 cycles
NICKS AND DENTS ON AIRCRAFT EXTERNAL SKIN BETWEEN FS 1000.00 - 1051.00, STGR 27 - 21R (C-CHECK RO 07/18/2025)REPAIRED NICKS AND DENTS ON AIRCRAFT EXTERNAL SKIN BETWEEN FS 1000.00 - 1051.00, STGR 27 - 21R IAW REO 670-53-61-2490, REV-- , DATE.2025-04-17. COMPLIED WITH ALL STEPS OF REO 670-53-61-2490, REV-- , DATE.2025-04-17. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: ROLLER — OUT OF LIMITS (ZONE 600 SLAT) · 24,946 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 RH - DISCARD THE RH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-630-824 (MRB 27-81-43-713), PART NUMBER: - , SERIAL NUMBER: 10132, POSITION: (C-CHECK RO 07/18/2025)REMOVED AND REPLACED SLAT TRACK 3-3 TOP FWD ROLLER WITH NEW P/N CC670-12567-1 REF CRJ700 AMM 27-81-43-000-805-A01 & AMM 27-81-43-400-806-A01OPERATIONAL CHECK OF THE FLAPS AND SLATS SYSTEM ACCOMPLISHED, REF CRJ 700 AMM 27-50-00-710-801-A02. CHECKS GOOD AT THIS TIMECOMPLIED WITH TASK CARD 27-630-824-A01
Part: ROLLER — OUT OF LIMITS (ZONE 500 SLAT) · 24,946 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 LH - DISCARD THE LH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-530-824 (MRB 27-81-43-713), PART NUMBER: - , SERIAL NUMBER: 10132, POSITION: (C-CHECK RO 07/18/2025)COMPLIED WITH TASK CARD 27-530-824 (CONFIG A01) - DISCARD OF THE LEFT TOP FORWARD SLAT-TRACK 3-3 ROLLERS. OPS CHECKED GOOD AT THIS TIME.COMPLIED WITH TASK CARD 27-900-1009-SKY (2EA)
Part: HINGE — WORN (ZONE 800) · 24,946 cycles
COMPLY WITH: 670BA-32-056 - LANDING GEAR - NOSE LANDING GEAR (NLG) AND DOORS - INSTALLATION OF A NEW HINGE FOR THE NLG AFT DOOR ASSEMBLY REV A PART(S) 0 (C-CHECK RO 07/18/2025)COMPLY WITH: SB 670BA-32-056 - LANDING GEAR - NOSE LANDING GEAR (NLG) AND DOORS - INSTALLATION OF A NEW HINGE FOR THE NLG AFT DOOR ASSEMBLY REV A DATED 04/17/2017 PART(S) 0"SERVICE BULLETIN 670BA-32-056, REVISION A, LANDING GEAR - NOSE LANDING GEAR (NLG) AND DOORS - INSTALLATION OF A NEW HINGE FOR THE NLG AFT DOOR ASSEMBLY, INCORPORATED" COMPLIED WITH REO 670-53-11-651 REV -B DATED 2025-04-16 14 FLAG NOTE 4 (A-C) COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Earlier reports · 2004–2024 · 177 reports
2024
Part: PRESSURE DECK — MECHANIC ERROR (ZONE 200) · 24,946 cycles
MAIN POST ASSEMBLY PN 53310-3 WAS MISDRILLED ON PRESSURE FLOOR, RESULTING IN MIS-LOCATED HOLES. INSTALLED NEW REINFORCMENT BRACKETS AND COMPLIED WITH ALL STEPS OF REO 670-53-41-706 REV --. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. LEAK CHECKED GOOD.
Part: STRINGER — OUT OF LIMITS (ZONE 800) · 24,946 cycles
COMPLY WITH: 670BA-53-040 - FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR REV C PART(S) B (C-CHECK RO 07/18/2025)SERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF THE LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART B, INCORPORATED AND COMPLIED WITH REO 670-53-21-493 REV -D DATE 2015-07-10 COMPLIED WITH 51-900-1002 SKY WEIGHT ADDED 0.3 LBS
2016
Part: UNKNOWN — ODOR (CABIN) · airframe 30,285 hrs · 21,638 cycles
ELECTRICAL ODOR DURING DECENT APPROX 15000 F/A NOTIFIED COCKPIT OF AN ELECTRICAL SMOKE ODOR. NO SMOKE WAS SEEN. TURNED OFF RECIRCULATION FAN, SMELL WAS STRONGER IN ROWS 1-5. A NON REV PILOT ACKNOWLEDGED ODOR AT ROW 12. REMOVED ELECTRICAL LOADS ALL WAS NORMAL. PERFORMED OPERATIONAL TEST OF CABIN LIGHT IAW AMM 33-21-00 NO DEFECTS NOTED AT THIS TIME COULD NOT DUPLICATE NO ELECTRICAL BURNING ODORS NOTED. ACFT OK FOR SERVICE.
Part: DOOR — UNKNOWN (MAIN PAX) · airframe 30,248 hrs · 21,607 cycles
PAX DOOR COULD NOT BE OPENED FROM THE INSIDE ACFT. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,222 hrs · 21,586 cycles
12 CD LOWER EXIT SING HAVE 2 LIGHT BULBS BURNED. REMOVED AND REPLACED 12 CD LOWER EXIT SIGN BULBS IAW AMM 33-24-07 OPS CHECK GOOD.
Part: CHARGER — FAILED (CABIN) · airframe 30,080 hrs · 21,459 cycles
GALLEY EXIT SIGNS FOR PAX DOOR INOPERATIVE. R & R NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-17. OPS CK GOOD. IPC REF 33-51-17, FIG, ITEM 8.
Part: DOOR — JAMMED (CABIN) · airframe 30,080 hrs · 21,459 cycles
CATERING CAN NOT OPEN SERVICE DOOR.
Part: GAS CYLINDER — OUT OF ADJUST (PAX DOOR) · airframe 29,839 hrs · 21,259 cycles
PASSENGER DOOR COULD NOT BE OPEN BY F/A GROUND CREW HAD DIFICULTY CLOSING AND OPENING DOOR HAD PROXIMITY SYSTEM 1 FAULT STATUS MESSAGE, DOORS AND OVERWING EMERGENCY EXITS. ADJUSTED FWD ASD GAS SPRING, OPS CK GOOD IAW AMM 52-11-17.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 29,634 hrs · 21,104 cycles
CENTER AISLE OVERHEAD MAIN, SERVICE DOOR EMERGENCY EXIT SIGN WILL NOT LIGHT UP. FOUND CONNECTORS TO EMERGENCY EXIT SIGNS LOOSE SECURED CONNECTORS. OPS CHECK GOOD IAW MM 33-51-07.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 29,308 hrs · 20,830 cycles
THE MEGAPHONE LOCATED IN THE AFT CABIN WAS FOUND TO BE INOP DURING THE LINE CHECK. THE MEGAPHONE LOCATED IN THE AFT CABIN WAS FOUND TO BE INOPERATIVE DURING THE LINE CHECK. R & R WITH SERVICEABLE MEGAPHONE BY PLACING IN MOUNT WITH VELCRO STRAP IN THE LAST, LT OVERHEAD BIN IPC 25-61-14, NR 5.
Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 29,308 hrs · 20,830 cycles
AFT CARGO BAY DOOR SILL IS CORRODED IN MULTIPLE AREAS. EVLAUATED AFT CARGO BAY DOOR SILL CORROSION AND FOUND TO BE OUT OF ALLOWABLE DAMAGED LIMITS OF SRM 53-61-23-101-00-A01. CORROSION DAMAGE BEYOND REPAIR. REMOVED AFT CAGO DOOR SILL IAW SRM 51-41-02-001-001-A01 AND 51-42-06-001-001-A01. REMOVED AFT CARGO DOOR LOWER SURROUND COMBING IAW SRM 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE CARGO DOOR SILL IAW SRN 51-42-06-001-001-A01 AND DWG AMM 670-35085.
Part: FRAME — CORRODED (BS 333) · airframe 29,308 hrs · 20,830 cycles
ATTACHING FLANGE AT FS 333.00, STR 26R TO 25R IS CORRODED. FRAME FLANGE AT FS 333.00 STR 26R-25R IS CORRODED. REMOVED CORROSION ON FRAME FLANGE AT 333.00 IAW SRM 51-21-06-001-001-A01. EVALUATED BLEND AREA AND FOUND BLEND INTO THE RADIUS OF ATTACH FLANGE AND WEB FOUND OUT OF ALLOWABLE DAMAGE LIMITS REF: SRM 53-21-06-101-002-A01. COMPLIED WITH REO EC/TC 670-53-21-799-03. CUTOUT FRAME 333, FROM STR 25L-25R IAW SRM 51-24-36-001-001-A01. FABRICATED AND INSTALLED REPAIR SECTION IAW REO 670-53-21-799-03. EC/TC REO 670-53-21-1261 AND REO 670-53-21-12-61 RECEIVED AND COMPLIED WITH.
Part: GUSSET — CORRODED (BS 280) · airframe 29,308 hrs · 20,830 cycles
GUSSET AT BS 280, LBL 12 CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG CC670-33052.
Part: STRIKER — CORRODED (DOOR SEAL) · airframe 29,308 hrs · 20,830 cycles
SERVICE DOOR LOWER SEAL STRIKER IS CORRODED AT ALL SCREW HOLES. REMOVED S/D LOWER SEAL STRIKER IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED S/D LOWER SEAL STRIKER IAW SRM 51-40-11-001-001-A01. INSTALLED S/D LOWER SEAL STRIKER IAW SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 29,308 hrs · 20,830 cycles
RIGHT SIDEWALL SEAT TRACK SEGMENT, BS 379-485 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-000-801-A01.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 29,308 hrs · 20,830 cycles
RIGHT SIDEWALL SEAT TRACK SEGMENT, BS 708-761.85 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-597) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 485-597 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-000-801-A01.
Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 29,308 hrs · 20,830 cycles
RIGHT SIDEWALL SEAT TRACK SEGMENT BS 597-677 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 597-677 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-000-801-A01.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 677-708 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-400-801-A03, AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 29,308 hrs · 20,830 cycles
RIGHT SIDEWALL SEAT TRACK SEGMENT BS 677-708 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-400-801-A03, AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 785.15 - 863 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 708-761.85 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 29,308 hrs · 20,830 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT HAS CORROSION BS 379-485. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,308 hrs · 20,830 cycles
RIGHT SIDEWALL SEAT TRACK SEGMENT BS 785-863 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. 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 485-581) · airframe 29,308 hrs · 20,830 cycles
RT SEAT TRACK SEGMENT BETWEEN BS 485 AND 581 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 29,308 hrs · 20,830 cycles
LEFT SEAT TRACK SEGMENT BETWEEN BS 485 AND 581 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 350-485) · airframe 29,308 hrs · 20,830 cycles
RT SEAT TRACK SEGMENT BETWEEN BS 350 AND 485 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 29,308 hrs · 20,830 cycles
LEFT SEAT TRACK SEGMENT BETWEEN BS 581- 677 HAS CORROSION IN MULTIPLE AREAS. SEAT TRACK OUT OF LIMITS IAW REO 670-53-00-013. REPAIRED IAW EC/TC REO 670-53-00-343. C REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03, 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 29,308 hrs · 20,830 cycles
RT SEAT TRACK SEGMENT BETWEEN BS 581 AND 677 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.
Part: SEAT TRACK — CORRODED (BS 374) · airframe 29,308 hrs · 20,830 cycles
LEFT SEAT TRACK SEGMENT HAS CORROSION AT BS 374. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.
Part: FITTING — CORRODED (BS 278) · airframe 29,308 hrs · 20,830 cycles
JACK SUPPORT FITTING AT FS 278.00 AND BL0.00 CORRODED. LT FWD AJCK SUPPORT FITTING CORRODED THRU ATTACH FLANGE AND CRACKED RT FWD JACK SUPPORT FITTING CORRODED ENTIRE LENGTH OF ATTACH FLANGE SERVICE INTERGRANULATE CORROISON ON INTERCOSTAL REQUIRES REPLACEMENT. LOCATED HOLES IN NEW JACK SUPPORT SRM 51-40-44-001-001-A01. REMOVED BOTH LT AND RT JACK SUPPORT INTERCOSTALS IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED LT AND RT JACK SUPPORT INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 REF DWG CCC70-32179.
Part: STRINGER — CORRODED (BS 319-349) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON STRINGER 26R BETWEEN FS 319.7 - 349. BLENDED DAMAGE BETWEEN FS 319 & FS 349 FOUND DEEP PITTING TO BE OUT OF LIMITS REF SRM 53-21-03-101-002-A01. REMOVED CLEATS AT FS 319, FS 333, FS 349 IAW SRM 51-42-0-001-001-A01. REMOVED STRINGER CLEATS ON THE FWD AND AFT FACE OF FRAME 295. REMOVED STRINGR FROM FS 280- FS 349, REMOVED 42 EA RIVETS AT DS 295 TO 349 TO FOM, IAW SRM 51-42-06-001-001-A01. DRILLED UP NEW STG 26R FWD AND AFT PIECES FROM FS 280-364 AND SPLICE ANGLE REF SRM 51-40-11-001-001-A01. INSTALLED STR 26R BETWEEN FS 280 AND FS 364 AND INSTALLED STR SPLICE AT FS 333 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-0A01 IAW DWG SH670-31630 AND SH670-32420. COMPLETED INSTALLATION OF INTERCOSTAL BETWEEN FS 349-FS 364 AND CLEATS IAW SRM 51-42-06-001-001-A01.
Part: DIAPHRAGM — CRACKED (BS 909) · airframe 29,308 hrs · 20,830 cycles
FUSELAGE EXTERNAL DIAPHRAM AT STR 24L FS909.00 IS CRACKED. RECEIVED & COMPLIED WITH EA 15-216-006, P4. REPAIRED IAW REO 670-53-82-487. COMPLIED WITH REO 670-53-82-478, R-A DATED 11-12-2014. REPAIRED WING FUSELAGE AFT FAIRING SUP FS 909.00, LBL 17.63 IAW REO 670-53-82-478.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON RT FLOORBEAM AT RBL 45 AND FS 280.00. REMOVED CORROSION IAW 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.
Part: FLOOR SUPPORT — CORRODED (BS 350) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON RT FLOOR SUPPORT AT BS 350 AND RBL 45. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: ANGLE — CORRODED · airframe 29,308 hrs · 20,830 cycles
CORROSION ON PAX DOOR SILL ANGLE. REMOVED UPPER MID-CAP ANGIE AT PAX DOOR IAW SRM 51-41-02-001-001 A01. INSTALLED UPPER MID CAP ANGLE IAW SRM 51-41-02-001-001-A01. LOCATED AND DRILLED NEW SERVICABLE MIDCAP ANGLE IAW SRM 51-40-11-001-001 A01. REMOVED LOWER PAX DOOR SILL IAW SRM 51-42-06-001-001 A01. INSTALLED SERVICABLE PAX DOOR LOWER SILL IAW SRM 51-42-06-001-001 A01 AND BOMBARDIER DRAWING SH670-31810. LOCATED AND DRILLED NEW SERVICABLE PAX DOOR LOWER SILL IAW SRM 51-40-11-001-001 A01. RECEIVED AND COMPLIED WITH EC/TC EA 26-2016-032.
Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON SERVICE DOOR SILL AT VARIOUS LOCATIONS ALONG THE SURFACE FROM FS 319.70 - FS 349.00. REMOVED S/D SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW S/D SILL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW S/D SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON COCKPIT FLOORBEAM ANGLE AT FS 280 BETWEEN RBL9-LBL9. REMOVED CORRODED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED, TRANSFERED, DRILL MOUNTING HOLES AND INSTALLED SERVICABLE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-48-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG CCG670-34010.
Part: FRAME — CORRODED (BS 280) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BETWEEN STR 26L-24R. BLENDED CORROSION ON CIRCUMFIRENTIAL JOINT AT S 280 BETWEEN STR 26L-24R. COMPLIED WITH EA 26-2016-024 SECTION 1-PERMANENT REPAIR.
Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 29,308 hrs · 20,830 cycles
CORROSION ON RT FLOOR SUPPORT AT FS 319.70 AND RBL 45. BLENDED CORROSION IAW 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.
2015
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,554 hrs · 20,228 cycles
12 AB LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,554 hrs · 20,228 cycles
12CD LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.
Part: UNKNOWN — SMOKE (LAVATORY) · airframe 28,239 hrs · 19,979 cycles
AFTER TAKEOFF, RECEIVED AFT SMOKE LAV, ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED. COMPLIED WITH COMPARTMENT WASH, DRY-OUT RUNS IAW AMM 72-00-00. ACFT OK FOR SERVICE.
Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,695 hrs · 19,547 cycles
EMERGENCY LIGHTS ON WHILE ARMED. CIRCUIT BREAKER RESET SYSTEM POWER TO EMERGENCY LIGHTS IAW FIM PG 12 FAULT NO LONGER EXIST IAW MCC NO FURTHER ACTION IS REQUIRED.
2014
Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 26,550 hrs · 18,685 cycles
NR 1 HYD QUANTITY EVACUATED IN FLIGHT TO 0 PERCENT. EDP RAN 1 HOUR 1 MIN W/OUT FLUID, EMERGENCY DECLARED AS A PRECAUTION. R & R LT ENGINE HYD PUMP IAW AMM 29-11-01, REF AIPC 29-11-01, ITEM 5. OPS AND LEAK CHECKS GOOD AT THIS TIME. ACFT RETURNED TO SERVICE. SDR CLOSED.
Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 26,050 hrs · 18,305 cycles
FWD CARGO DOOR SEAL RETAINER BENT AT FWD SIDE. REPAIRED IAW EC/TC REO 670-52-35-127 01 FOR PERMANENT REPAIR TO THE FWD CARGO DOOR SEAL LOWER RETAINER.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 25,780 hrs · 18,103 cycles
FWD EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. R & R FWD EMERGENCY LIGHT BATTERY IAW AMM 33-51-17. OPS CHECKED GOOD.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,323 hrs · 17,742 cycles
WHILE INVESTIGATING COFFEEMAKER, FOUND HEAT DAMAGE TO FUSELAGE SKIN ABOVE GALLEY 1. PERFORMED VISUAL INSPECTION FOR BUCKLING OR WARPING IAW SRM 51-11-06 NO DEFECTS NOTED. CLEANED DAMAGED AREAS IAW SRM 51-26-00.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,929 hrs · 17,440 cycles
CABIN SECOND FROM FRONT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00.
Part: LINKAGE — UNSECURE (SERVICE DOOR) · airframe 24,873 hrs · 17,400 cycles
SERVICE DOOR WILL NOT OPEN. SECURED LINKAGE ON SERVICE DOOR LATCH IAW AMM 52-41-03. OPS CHECKED GOOD IAW AMM 52-41-00. ACFT OK FOR SERVICE.
Part: SKIN — DAMAGED (WING) · airframe 24,587 hrs · 17,189 cycles
FOUND 1EA OVERSIZED HOLE IN WING SKIN AND ONE FREEZE PLUG ON LT SIDE. COMPLIED WITH REO 670-57-21-658, REV (P1). MAJOR REPAIR.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 24,587 hrs · 17,189 cycles
FOUND LEFT COCKPIT FLOOR SUPPORT AT FS 280 ANGLE CRACKED AND GUSSET UNSERVICEABLE. REMOVED LT COCKPIT FLOOR SUPPORT ANGLE AND GUSSET IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED ASSEMBLED NEW SUPPORT ANGLE AND GUSSET IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE & GUSSET AT FS 280 IAW SRM 51-42-06-001-001 & 51-42-10-001-001, DWG CC670-33467. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,584 hrs · 17,186 cycles
WHILE PERFORMING SB 670BA-53-041, FOUND RT COCKPIT BS 280 FLOORBEAM ANGLE CRACKED AND GUSSET UNSERVICEABLE. REMOVED FLOORBEAM ANGLE AND GUSSET IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED AND ASSY NEW FLOORBEAM ANGLE AND GUSSET IAW SRM 51-40-11-001-001-A01 AND INSTALLED IAW SRM 51-42-06-001-001-A01 AND DWGCC670-33199.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 24,587 hrs · 17,189 cycles
LT COCKPIT FLOORBEAM FOUND CRACKED. REPAIRED IAW REO 670-53-11-893, REV "B".
2013
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,584 hrs · 17,186 cycles
RT 280, LOWER BULKHEAD WEB CORRODED. REPAIR RT LOWER BULKHEAD WEB IAW SRM 53-11-10-201-003-A01. REPAIR "A" IF BEYOND LIMITS OF REPAIR "A" REPAIR IAW GREO. HAND BLENDED AREAS OF CORROSION & FOUND AREAS, WITHIN LIMITS, IAW SRM 53-11-10-201-003-A01 & TREATED IAW SRM 51-21-16-001-001. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 693) · airframe 24,584 hrs · 17,186 cycles
SEAT TRACK CORRODED BS 693 RBL 9. REMOVED DAMAGED SEAT TRACK IAW AMM 53-00-49-000-801-803. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 549) · airframe 24,584 hrs · 17,186 cycles
SEAT TRACK CORRODED AT BS 549. R & R SEAT TRACK IAW AMM 53-00-49-400-801.
Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 24,587 hrs · 17,189 cycles
RT FLOOR SUPPORT CORRODED BS 280 - 319.7. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. 100 PERCENT MATERIAL LOSS AT 3 LOCATIONS IS BEYOND LIMITS OF SRM 53-00-00-101-001-A01. REMOVED FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01 AND DWG SH670-32170. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND DWG.
Part: POST — CORRODED (BS 280) · airframe 24,587 hrs · 17,189 cycles
LEFT 280 WEB POST CORRODED AT BOTTOM. REMOVED CORROSION IAW SRM 51-21-06-001-01-A01. RESTORED FINISH IAW SRM 51-25-16-001-001.
Part: TRACK — DENTED (CARGO DOOR) · airframe 24,587 hrs · 17,189 cycles
AFT BAGGAGE BAY FWD AND AFT DOOR TRACKS HAVE DENTS. REPLACED DOOR TRACKS IAW REO 670-53-62-0102. MAJOR REPAIR.
Part: DOUBLER — CHAFED (RT NACELLE) · airframe 24,587 hrs · 17,189 cycles
RIGHT ENGINE LOWER CORE COWL, INNER SKIN DOUBLE REPAIR HAS CHAFE DAMAGE. REMOVED DOUBLER ON RT LOWER COWL DOOR IAW SRM 51-42-06-001-001. COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,587 hrs · 17,189 cycles
LEFT 280 BULKHEAD WEB CORRODED. REMOVED CORROSION & FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,584 hrs · 17,186 cycles
FLOORBEAM ANGLE AT FS 280 CORRODED. R & R FLOORBEAM ANGLE IAW DWG CC670-334010, REV H, SRM 51-42-15-001-001-A01, 51-42-21-001-001-A01, & 51-42-06-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,584 hrs · 17,186 cycles
BS 280 FLOORBEAM CORRODED. REMOVED AND INSTALLED NEW, DURING INCORPATION OF SB 670BA-53-041, PART A.
Part: POST — CORRODED (BS 280) · airframe 24,587 hrs · 17,189 cycles
RT 280 WEB POST CORRODED AT BOTTOM. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. RESTORED FINISH IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-21-16-001-001-A01 AND DWG CC670-34010.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,584 hrs · 17,186 cycles
FLOORBEAM ANGLE BS 280 CORRODED. R & R WITH A NEW ANGLE DURING INCORPORATION OF SB 670BA-53-041, PART A.
Part: DOUBLER — CHAFED (BS 977) · airframe 24,587 hrs · 17,189 cycles
FUSELAGE SKIN DOUBLER AT STRINGER 27 BS 977 HAS CHAFE DAMAGE FROM CHANNEL ON PANEL 195DL/196DR AND SCREW INDENTIONS. REPAIRED IAW REO 670-53-00-290. MAJOR REPAIR.
Part: STRUCTURE — CRACKED (TRU BAY) · airframe 24,584 hrs · 17,186 cycles
LEFT TRU BAY STRUCTURE CRACKED AT BS 193. COMPLIED WITH REO PL 670-53-11-509. MAJOR REPAIR.
Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 24,530 hrs · 17,147 cycles
EMERGENCY LIGHT LENS DISCOLORED. R & R LIGHT LENS IAW AMM 33-51-05.
2012
Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 22,056 hrs · 15,384 cycles
AT 4000 FT, RUDDER IMMEDIATLEY WENT FULL LT, RUDDER TRIM ATTEMPTED TO TRIM BACK TO RT AND TRIM WENT FULL RT TRIM, TRIM CONTINUED TO MOVE UNCOMMANDED AND FINALLY STOPPED AT HALF RT RUDDER TRIM. AUTO PILOT WAS NOT ENGAGED. ACFT RETURNED TO DEPARTURE AFTER T/O. R & R TRIM CONTROL PANEL IAW AMM 27-12-10. PERFORMED OP TEST IAW AMM 27-11-00-710-802. NO FAULTS FOUND AT THIS TIME.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,789 hrs · 15,184 cycles
CEILING EMERGENCY LIGHT OUT AT 17ABCD. LAMPED IAW AMM 33-51-09.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,834 hrs · 14,472 cycles
F/A MEGAPHONE INOPERATIVE. R & R F/A MEGAPHONE IAW AMM 25-61-14, REF IPC 25-25-61-14, ITEM 5, OPS TESTED GOOD.
2011
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 19,770 hrs · 13,738 cycles
EMERGENCY LIGHTS INOPERATIVE. FOUND BURNED OUT FUSE IN NR 1 ESPU BATTERY CHARGER. REMOVED NR1 ESPU BATTERY CHARGER IAW AMM 33-51-17-00-802. REMOVED NR 1 BATTERY CHARGER IAW AMM 33-51-17-00-802. INSTALLED NEW NR 1 ESPU BATTERY CHARGER REF AMM 33-51-17-400-802.
Part: SUPPORT — DAMAGED · airframe 19,770 hrs · 13,738 cycles
DURING REMOVAL OF FUEL CAP FOR O-RING REPLACEMENT, DAMAGE TO THE LIGHTNING HOLE OCCURED. FABRICATED MOUNTING SUPPORT AND MOUNTING SUPPORT AFT IAW SRM 51-24-16-001-001-A01, 51-24-21-001-001-A01, 51-24-36-001-001-A01, AND DWS SH670-3967-5 AND SH670-39065-5. INSTALLED FABRICATED PARTS SRM AND DWGS.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
SERVICE DOOR THRESHOLD MOUNTING BRACKET CORRODED. FABRICATED ANGLE AND INSTALLED IAW EO 700-53-0224.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
CABIN SERVICE DOOR LOWER ANGLE CORRODED.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
CABIN SERVICE DOOR THRESHOLD MOUNT ANGLE CORRODED. REPAIRED IAW REO 670-53-21-775.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
CABIN SERVICE DOOR THRESHOLD MOUNT ANGLE CORRODED.
Part: SILL — CHAFED (CARGO DOORWAY) · airframe 19,770 hrs · 13,738 cycles
AFT CARGO DOOR SILL PLATE CHAFED. REPAIRED IAW REO 670-53-61-808.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 19,770 hrs · 13,738 cycles
CABIN SERVICE DOOR LOWER SILL ANGLE CORRODED. BLENDED CORRODED AREA AS REQUIRED TO REMOVE DAMAGE IAW SRM 51-21-06-001-001-A01- WA161715. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06-001-A01. INSTALLED LOWER SILL ANGLE.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
CABIN SERVICE DOOR THRESHOLD MOUNT ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3, MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL REMOVED IS .002" AREA OUT OF LIMITS IAW SRM 53-21-23-101-002-A01, PARA 3B (1). COMPLIED WITH STEP 2 OF REO 670-53-21-775 IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED AT THIS TIME.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODED AND FOUND TO BE WITH IN LIMITS. REMOVED RT SIDE SIDE SEAT TRACK FROM FS 677 TO 708 IAW AMM 53-00-49-000-801-A03. INSTALLED RT SIDE SEAT TRACK FROM FS677 TO FS708 IAW AMM 53-00-49-400-801. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW MAC NDT INSPECTION PROCEDURE PT-1 IAW SRM 51-12-00-001-001-A01. NO INDICATIONS NOTED. APPLIED CORROSION PREVENTATIVE TREATMENT AS PRESCRIBED BY SRM 53-31-49-001-A01 AND SRM 51-21-16-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 19,770 hrs · 13,738 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION FROM FS 485-565 IN SEVERAL PLACES. (OPEN)
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 19,770 hrs · 13,738 cycles
RIGHT SIDE SEAT TRACK FROM FS 677 TO 708 CORRODED IN SEVERAL PLACES. (OPEN)
Part: FRAME — CORRODED (COCKPIT) · airframe 19,770 hrs · 13,738 cycles
FOUND COCKPIT LOAD TO BE CORRODED BEYOND LIMITS IAW SRM 51-21-06. LOCATED HOLES IN NEW COCKPIT LAND AND INSTALLED. ALL WORK DONE IAW SRM 51-42-00-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-23-001-001-A01. MINOR REPAIR.
Part: SKIN — CORRODED (BS 295-310) · airframe 19,770 hrs · 13,738 cycles
CORROSION OF FUSELAGE SKIN UNDER TCAS OMIN DIRECTIONAL ANTENNA S27 BETWEEN FS 295 & 310. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PRODURE RT-3. NO LOSS OF MATERIAL FOR LIGHT CORROSION. RESTORED FINISH IAW SRM 51-21-05-001-001-A01, PARA 3B4 AND 5. MINOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 19,770 hrs · 13,738 cycles
LEFT SIDE SEAT TRACK FROM FS 785-863 CORRODED IN SEVERAL PLACES. (OPEN)
Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,770 hrs · 13,738 cycles
FOUND FLOORBEAM TO BE CORRODED BEYOND LIMITS IAW SRM 51-21-06. REMOVED AND REPLACED BS 280 FLOORBEAM IAW REO 670-53-11-047.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODED. REMOVED RT SIDE, SIDE SEAT TRACK FROM FS785 TO FS863 IAW AMM 53-00-49-000-801-A03. BLENDED RT SIDE SEAT TAIL DAMAGE FOUND TO BE OUT OF LIMITS REF SRM 53-51-49-101-001. INSTALLED NEW RT SIDE SEAT TRACK IAW SRM 53-00-49-400-801.
Part: FLOOR PANEL — CORRODED (BS 280) · airframe 19,770 hrs · 13,738 cycles
AFT COCKPIT FLOOR 1 AND ON FS 280 CORRODED. (OPEN)
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODED, REMOVED SEAT TRACK FROM FS 708 - 761 IAW AMM 53-00-49-000-801-A03. INSTALLED SEAT TRACK IAW AMM 53-00-40-400-801(A03).
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 19,770 hrs · 13,738 cycles
LEFT FLOOR SEAT TRACK FROM FS 581 TO 677 HAS SEVERAL CORRODED SPOTS.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 19,770 hrs · 13,738 cycles
CORROSION EVALUATED TO BE WITHING LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED LT SIDE SEAT RAIL FROM FS 863 FS 977 IAW AMM 53-00-49-000-801. INSTALLED LT SIDE SEAT RAIL ON FS 863 & 977 IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 19,770 hrs · 13,738 cycles
RT SIDE SEAT TRACK HAS MINOR CORROSION FROM FS 565-661 IN SEVERAL PLACES. EVALUATED RT SEAT TRACK AND FOUND TO BE OUT OF ALLOWABLE LIMITS 2 LUGS OR LANDS ARE COMPLETELY BLENDED AWAY. REMOVED RT SIDE SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED RT NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,770 hrs · 13,738 cycles
280 CROSSBEAM CORRODED ON LT SIDE TOP AND CENTER SECTION. (OPEN)
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 19,770 hrs · 13,738 cycles
RIGHT SIDE SEAT TRACK FROM FS 708-761 CORRODED IN SEVERAL PLACES. (OPEN)
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODED, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODEDFROM FS 485 TO 565 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-41-49-101-001-A01. .110 MATERIAL REMAINING .102, REMOVED .008. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW MAC NDT INSPECTION PROCEDURE PT-1 IAW SRM 51-12-00-001-001-A01. NO INDICATIONS NOTED. APPLIED CORROSION PREVENTATIVE TREATMENT AS PRESCRIBED BY SRM 53-31-49-001-A01 AND SRM 51-21-16-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,770 hrs · 13,738 cycles
RIGHT SEAT TRACK FROM FS 485 TO 581 CORRODED IN SEVERAL SPOTS. REMOVED RT FLOOR SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485) · airframe 19,770 hrs · 13,738 cycles
SEAT TRACK CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-31-491. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK, FS 485 TO FS 581 SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 646) · airframe 19,770 hrs · 13,738 cycles
REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-31-49. REMOVED SEAT TRACK FROM FS 581 TO FS 677 IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-403.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 19,770 hrs · 13,738 cycles
LEFT SIDE SEAT TRACK FS 708-761 CORRODED IN SEVERAL PLACES. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 19,770 hrs · 13,738 cycles
RIGHT SIDE SEAT TRACK FROM FS 785-863 CORRODED. (OPEN)
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 19,770 hrs · 13,738 cycles
RT FLOOR SEAT TRACK FROM FS 581-677 CORRODED OUT OF LIMITS. REMOVED RT FLOOR SEAT TRACK AND INSTALLED WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
Part: BRACKET — CORRODED (THRESHOLD) · airframe 19,770 hrs · 13,738 cycles
SERVICE DOOR THRESHOLD MOUNTING BRACKETS CORRODED. BLEND BRACKETS IAW SRM 51-21-06-001-001 ORIGINAL MATERIAL .063 MATERIAL REMAINING IS .039 & .038. FOUND TO BE OUT OF LIMITS SRM 53-21-23. FABRICATED BRACKETS IAW SRM 51-24-36-001-001-A01. TREATED, PRIMED, AND PAINTED BRACKETS IAW AMM 51-21-01-380-801, SRM 51-258-06-001-001-A01, 51-25-21-00-001-A01. INSTALLED BRACKETS IAW SRM 51-42-06-001-A01.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,770 hrs · 13,738 cycles
LT SIDE SEAT TRACK HAS MINOR CORROSION FROM FS 379-485. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 19,770 hrs · 13,738 cycles
LEFT SIDE SEAT TRACK FROM FS 863-977 CORRODED IN SEVERAL PLACES. (OPEN)
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,770 hrs · 13,738 cycles
LT FLOOR SEAT TRACK FROM FS485 TO 581 HAS SEVERAL CORRODED SPOTS. (OPEN)
Part: SKIN — CORRODED (BS 295) · airframe 19,770 hrs · 13,738 cycles
MINOR CORROSION AFT OF FS 295 AT STRINGER 27 AROUND ANTENNA FITTING. REMOVE CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .047" ORIGINALS .050". .003" MATERIAL REMOVED. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-21-01-101-002-A01. REPAIRED IAW REO 670-53-21-772.
Part: PLACARD — BROKEN (PAX DOOR) · airframe 19,770 hrs · 13,738 cycles
PAX DOOR INNER HANDLE EXIT/PULL SIGN BROKEN. (OPEN)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,770 hrs · 13,738 cycles
EMERGENCY LIGHT INOPERATIVE, REMOVED EMERGENCY LIGHT AND REPLACED WITH NEW SERVICEABLE LIGHT ASSY IAW AMM 33-51-01-400-801. OPS CHECKED GOOD IAW AMM 33-51-01-710-801.
Part: LIGHT — DAMAGED (CABIN) · airframe 19,770 hrs · 13,738 cycles
LEFT EMERGENCY LIGHT MISSING COVER AND TAPE IS CRACKED AND PARTS ARE MISSING. (OPEN)
Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 19,770 hrs · 13,738 cycles
LT EMERGENCY FLOOR PATH TRACK NR 8 COVER IS HAZED.
Part: LIGHT — DAMAGED (CABIN) · airframe 19,770 hrs · 13,738 cycles
RT EMEGENCY LIGHT NR 7 COVER IS HAZED AND ARE STAINED AND CRACKED. (OPEN)
Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 19,770 hrs · 13,738 cycles
LEFT EMERGENCY FLOOR PATH TRACK NR 7 COVER IS HAZED AND PARTS OF THE PHOTO LUMINECENT TAPE ARE STAINED.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,770 hrs · 13,738 cycles
ANGLE CRACKED ON AFT SIDE OF ASD BY ASSIST MOTER PULLEY. R & R DRAG ANGLE REPAIR SPLICE IAW SRM 51-42-06-001-001-A01. MINOR REPAIR.
Part: MEGAPHONE — BROKEN (CABIN) · airframe 19,439 hrs · 13,508 cycles
MEGAPHONE BROKEN. RESECURED MEGAPHONE ASSY TOGETHER AS REQUIRED. OPS CHECKED GOOD IAW AMM 25-61-14.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,276 hrs · 12,694 cycles
EXIT SIGN LENS COVER NEAR SERVICE DOOR BESIDE GALLEY CONTAINERS MISSING. REPLACED LIGHT COVER IAW AMM 33-51-10.
2010
Part: PLACARD — DETERIORATED (CABIN) · airframe 17,009 hrs · 11,833 cycles
ASD "EXIT" AND "RED ARROW" PLACARDS ARE DETERIORATED. R & R ASD "EXIT" AND "RED ARROW" PLACARDS IAW CRJ700 20-60-04. (CLOSED)
Part: SIGN — MISSING (CABIN) · airframe 16,770 hrs · 11,651 cycles
EMERGENCY EXIT LIGHT COVER AT FLOOR LEVEL NEAR SERVICE DOOR MISSING. REPLACED EMERGENCY EXIT LIGHT SIGN AND COVER NEAR SERVICE DOOR IAW AMM 33-51-05. OPS CK GOOD. (CLOSED])
Part: SIGN — DETACHED (CABIN) · airframe 16,492 hrs · 11,447 cycles
EXIT SIGN ATTATCHMENT IS NOT STAYING ATTATCHED IN EXIT ROW 12A. REPAIRED 12A EXIT DOOR HANDLE COVER IAW 25-60-00. OK FOR SERVICE.
Part: STEERING UNIT — MALFUNCTIONED (NLG) · airframe 16,487 hrs · 11,443 cycles
ON GEAR RETRACTION EICAS GENERATED STEERING INOP MESSAGE. CYCLED CB1 G2 & CB2 G2 AFTER LANDING. NOSE WHEEL STEERING RESET. (EMERGENCY DECLARED & EQUIPMENT REQUESTED TO BE STANDING BY) SYS RESET WITH NO FURTHER FAULTS. IAW SL32-019, REV C SYS, OPS OK IAW AMM 32-51-01.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,425 hrs · 11,396 cycles
F/A REPORT FWD F/A STATION FLASHLIGHT NOT ILLUMINATING WHEN SELECTED ON. REPLACED FLASH LIGHT IAW AMM 25-00-00. (CLOSED)
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,173 hrs · 11,211 cycles
MAIN CABIN INTERIOR GALLEY G-2 EMERGENCY FLOOD LIGHT LENS BROKEN. R & R G-2 GALLEY EMERGENCY FLOOD LIGHT LENS IAW AMM 33-51-11.
Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 16,172 hrs · 11,210 cycles
MAIN CABIN INTERIOR G-3 GALLEY EMERGENCY EXIT SIGN LENS CRACKED. INSTALLED SERVICEABLE EMERGENCY EXIT SIGN LOCATED ON NEW WARDROBE IAW AMM 33-51-05.
Part: LENS — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 16,172 hrs · 11,210 cycles
MAIN CABIN INTERIOR G-3 GALLEY EMERGENCY EXIT SIGN LENS. INSTALLED A SERVICABLE EMERGENCY EXIT SIGN LENS IAW AMM CHAP 33-51-05/ 56000122, P242.
Part: LENS — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 16,172 hrs · 11,210 cycles
WOO/10 MAIN CABIN INTERIOR G-2 GALLEY EMERGENCY FLOOD LIGHTS LENS. R & R G-2 GALLEY EMERGENCY FLOOD LIGHT LENS IAW MM 33-51-11.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,148 hrs · 11,186 cycles
BS 280 BEAM LT AND RT SIDE BADLY CORRODED. COMPLIED WITH EC/TC SB 670BA-53-026 REV.B.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
FWD LT 280 BRACKET PN BA670-30068-1 FOUND CRACKED. REMOVED CRACKED BRACKET PN BA670-30068-1 AND REPLACED WITH SERVICEABLE BRACKET PN BA670-30068-1 INSTALLED JO-BOLTS THROUGH OTBD SIDE OF BRACKET ALL WORK DONE IAW SRM 51-42-22-001-001-A01. CONTINUE INSTALLING LOCK FASTENERS IN BRACKET. FINISHED INSTALLING LOCK FASTENERS IN BRACKETS IAW SRM CH 51-42-21-001-001.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
SEAT TRACKS AT LBL 9 AND RBL 9 CORRODED. EVALUATED SEAT TRACKS AT LBL9 AND RBL9, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. SEAT TRACK LBL9 & RBL9 ARE TO BE REPLACED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
LT SIDE WALL SEAT TRACK NR 3 AFT OF ASD CORRODED. EVALUATED LT SIDE WALL SEAT TRACK NR 3 AFT OF ASD FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED LT SIDE WALL NR 3 SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
LEFT SIDE WALL SEAT TRACK NR 5 AFT OF ASD CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED LT SIDEWALL SEAT TRACK NR 5 REF IAW AMM TASK 53-00-49-000-801. INSTALLED LT SIDEWALL SEAT TRACK NR 5 REF AMM TASK 53-00-49-400-801. INSTALLED FASTENERS IN LT SIDEWALL SEAT TRACK NR 5 EXCEPT FOR 2 EA FASTENERS LOCATED AT FS 754.00 IAW AMM 53-00-49-000-801. INSTALL 2 FASTENERS WHEN RECEIVED. INSTALL 2 FASTENERS WHEN RECEIVED. COMPLETED INSTALLATION OF NR 5 LT SIDE SEAT TRACK BY INSTALLING 2 FASTNERS IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 16,148 hrs · 11,186 cycles
CENTER AISLE RT SIDE FLOOR TRACK CORRODED AT FS 349. EVALUATED CTR AISLE RT SIDE FLOOR TRACK FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 TR 53-0015. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. NSPECTED RT FLOORBEAM TITANIUM CAPS AT FS 349. FOUND NO CORROSION, INSTALLED CTR AISLE RT SIDE FLOOR TRACK AT FS 349 IAW AMM 53-00-49-400-801.
Part: BEAM — CORRODED (BS 280) · airframe 16,148 hrs · 11,186 cycles
BS 280 BEAM LT & RT SIDES BADLY CORRODED. ALL WORK DONE IAW SRM 51-42-06 AND SRM 51-42-21.
Part: SEAT TRACK — CORRODED (BS 370) · airframe 16,148 hrs · 11,186 cycles
CENTER AISLE LT SIDE SEAT TRACK CORRODED AT FS 370.0. EVALUATED CTR AISLE LT SIDE FLOOR TRACK AT FS 370 FOUND TO BE OUT OF LIMITS CORRODED. IAW SRM 53-21-49-101-001-A01 TR 53-0015. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSPECTED LT FLOORBEAM TITANIUM CAPS AT FS 370.00. FOUND NO CORROSION. INSTALLED SEAT TRACK (SERVICEABLE) IAW AMM TASK 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
LT SIDE WALL SEAT TRACK NR 2 FROM ASD CORRODED. EVALUATED LT SIDE WELL TRACK NR 2 FROM ASD, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, TR 53-0015, REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM TASK 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,148 hrs · 11,186 cycles
LEFT SIDE WALL SEAT TRACK NR 4 AFT OF ASD CORRODED. EVALUATED LT SIDEWALL SEAT TRACK NR 4 AFT OF ASD FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 TR 53-0015. SEAT TRACK NEEDS TO BE REPLACED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALL SERVICEABLE SEAT TRACK. INSTALLED LT SIDE WALL SEAT TRACK NR 4 IAW AMM 53-00-49-400-801.
Part: PLACARD — TORN (ESCAPE HATCH) · airframe 16,148 hrs · 11,186 cycles
CREW ESCAPE HATCH EMERGENCY EXIT PLACARD TORN. REPLACED PLACARD AT CREW ESCAPE HATCH EMERGENCY EXIT IAW AMM 20-60-11.
2009
Part: LIGHT — UNSECURE (CABIN) · airframe 14,246 hrs · 9,722 cycles
LEFT SIDE EMERGENCY FLOOR PATH MARKING BETWEEN FS 357.02 AND FS 374.58, (AT THE FWD LAV), UNSECURE.
Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 13,672 hrs · 9,293 cycles
EXTERNAL EMERGENCY LIGHT OVER RT WING IS VERY DIM.
Part: SPOILER SYS — MALFUNCTIONED · airframe 13,611 hrs · 9,248 cycles
OB FLTR SPLRS & OB SPOILERON CAUTION MSG ON DESCENT FROM ATL, MACH TRIM MESSAGE REPEAT WRITE UP WITHIN 2 LEGS. EMERGENCY DECLARED. FLT 5027, 5035 CX.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,474 hrs · 9,151 cycles
THE 2ND FROM FRONT CABIN CEILING EMERGENCY LIGHT INOP.
Part: TRIM SYSTEM — MALFUNCTIONED (STABILIZER) · airframe 13,168 hrs · 8,924 cycles
DESCENDING INTO ATL 30 MIN BEFORE LANDING THE STAB CH2 FAIL THEN IT RE-ENGAGED BY ITSELF. LATER THE MACH TRIM DISENGAGED AND BOTH STAB TRIM CHANNELS FAILED. STAB TRIM WENT TO "0" FULL DOWN. RAN QRH AND LANDED FLAPS 20. ON SHORT FINAL STAB TRIM 1 & 2 RE-ENGAGED BY ITSELF AND TRIM WENT TO 2.6, EMERGENCY DECLARED. FLT 5159 DEL 94 MINS.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,932 hrs · 7,994 cycles
LT FUSELAGE MIDDLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT FUSELAGE MIDDLE EMERGENCY LIGHT BULB. OPS CHECK GOOD. (S)
Part: BEARING — CRACKED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
RIGHT WING-TO-FUSELAGE ATTACH LINK AT FS 797.00 UPPER SPHERICAL BEARING CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
STRINGER 25RT CORRODED BETWEEN FS 295 AND FS 310 BLENDED STRINGER AND FOUND TO BE OUT OF LIMITS. REMOVED STRINGER SECTION FROM 290 - 310 PER SRM 51-42-06. INSTALLED NEW STRINGER, DRILLED HOLES TO SIZE, INSTALLED AFT FASTENERS FROM SPLICE TO SKIN PATCH PER SRM 51-42-06. INSTALLED FASTENERS INTO STRINGER 25RT FORWARD OF REPAIR DOUBLER IAW CRJ 700 SRM 51-42-06, SM 7023171 04-12-08, JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 4/21/08.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
STR 26RT CORRODED BETWEEN STA 333 AND 349. REMOVED AND REPLACED STRINGER PER SRM 51-42-06 AND 51-42-21.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
STRINGER 25 RT HAS CORROSION DAMAGE JUST AFT OF FS 333.00 IN MAIN AVIONICS BAY. REMOVED CORRODED STRINGER PER SRM 51-42-06, BLEND SPLICE FOUND TO BE OUT OF LIMITS. DRILLED AND INSTALLED NEW STRINGER SPLICE 25 RT PER SRM 51-40-11, 51-42-06 AND 51-42-21.
Part: SKIN — CORRODED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
FUSE SKIN CORRODED BETWEEN STA 295 AND 310 AND BETWEEN STRINGER 24RT AND 25RT. REMOVED CORROSION IAW SRM 53-21-01SP. MINIMUM SKIN THICKNESS OF .030, .017 BLEND DEPTH (37 PERCENT) IS OUT OF LIMITS OF SRM 53-21-01 AND 53-00-01 FIG 53-00-01-991-805. FABRICATED REPAIR DOUBLER. CUTOUT REQUIRES NDT PER SRM 53-00-01 PG 207. INSTALLED REPAIR DOUBLER, FAY SEALED AND APPLIED PRIMER TO REPAIR AREA PER SRM 53-00-01. PAINTED FASTENERS IN REPAIR AREA AND APPLIED CIC TO AREA PER SRM 51-21-00.
Part: DOOR — FAILED (EMERGENCY EXIT) · airframe 11,222 hrs · 7,483 cycles
RIGHT OVERWING EMERGENCY DOOR FAILED FUNCTIONAL CHECK.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,222 hrs · 7,483 cycles
COCKPIT FLOOR, AFT LAND IS CORRODED BEYOND LIMITS.
Part: PLACARD — LOOSE (CABIN) · airframe 11,222 hrs · 7,483 cycles
ASD 'EXIT' PLACARD COMING LOOSE. REPLACED PLACARD IAW AMM 11-30-02.
Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 11,222 hrs · 7,483 cycles
ASD EXTERNAL HANDLE CRACKED. REMOVED AND REPLACED DOOR HANDLE. ACCOMPLISHED IAW T/C SB670BA-52-030.
Part: STRUCTURE — CRACKED (ASD) · airframe 11,222 hrs · 7,483 cycles
ASD FWD SIDEWALL CRACKED AT 2ND STEP RISER.
Part: PLACARD — UNSECURE (CABIN) · airframe 10,674 hrs · 7,107 cycles
F/A REPORTS MAIN DOOR-EXIT PLACARD AND OPEN SIGN UNSECURED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,619 hrs · 7,067 cycles
CEILING LEVEL EMERGENCY LIGHT AT ROW 10 FAILED. FLT 4413 DEL 33 MINS. CABIN EMERGENCY LIGHTS, CEILING LEVEL FLOODLIGHTS.
2007
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,566 hrs · 7,037 cycles
LEFT EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 9,279 hrs · 6,176 cycles
MEGAPHONE NOT OPERATING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,112 hrs · 5,353 cycles
FOUND EMERGENCY CEILING LIGHT ABOVE ROW 10 INOP.
2006
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,902 hrs · 5,196 cycles
FWD FLOOR ANGLE AT FS 280 FROM LBL 9 TO RBL 9 IS CORRODED. WORK COMPLETE. REMOVED FLOOR SUPPORT ANGLE IAW SRM CH 51. DRILLED AND COUNTERSUNK NEW FLOOR SUPPORT ANGLE IAW CRJ 700 SRM CH 51. STARTED INSTALLING 280 FLOOR LAND BETWEEN RBL 9 AND LBL 9 AS REQUIRED IAW CRJ 700 SRM 51-42-06. FINISHED INSTALLING COCKPIT FLOOR LAND AND RECEPTICLES ON FWD SIDE OF 280 BEAM AS REQUIRED IAW CRJ 700 SRM 51-42-06. JOB COMPLETE. SUPPLEMENTAL.
Part: BEAM — CORRODED (BS 280) · airframe 7,902 hrs · 5,196 cycles
FS 280 BEAM CORRODED. REPAIRED IAW REO 670-53-11-047.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 7,902 hrs · 5,196 cycles
LT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE HAS POSSILBLE CRACK (MARKED).
Part: WEB — CORRODED (BS 280) · airframe 7,902 hrs · 5,196 cycles
RT SIDE FS 280 WEB CORRODED. REPAIRED PER ALL PERTINENT MATERIALS.
Part: WEB — CORRODED (BS 280) · airframe 7,902 hrs · 5,196 cycles
LEFT SIDE FS 280 WEB CORRODED. WORK COMPLETE. REMOVED LEFT SIDE FLOOR SILL HOSE CLAMP ASSY, REMOVED LEFT SIDE 280 BULKHEAD DOUBLER STRAP. STARTED REMOVING FASTENER COMMON TO THE 280 BULKHEAD AFT LOWER WEB IAW REO 670-53-11-052. REMOVED LEFT 280 WEB, REMOVED LEFT CABLE FAIRLEAD TO GAIN ACCESS, LOCATED EXISTING HOLES IN NEW LEFT 280 WEB IAW 670-53-11-052. CLECOED LEFT HAND WEB AND DOUBLER INTO PLACE IAW REO 670-53-11-052. FAYED SEALED LEFT WEB INTO LOCATION AND INSTALLED CLECO'S. BEGAN INSTALLING LEFT 280 WEB ALL WORK DONE IAW REO 670-53-11-052 DK 7022603,12-17-06. FINISHED INSTALLING LEFT WEB AND LEFT CABLE FAIRLEAD AS REQUIRED. ALL WORK COMPLETED IAW REO 670-53-11-052. JOB COMPLETE. SUPPLEMENTAL
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,902 hrs · 5,196 cycles
LOWER EMERGENCY EXIT LIGHT AT LEFT E/E HAS 1 BULB OUT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,570 hrs · 4,981 cycles
FUSELAGE RT AFT EMERGENCY LIGHT INOP.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,782 hrs · 4,497 cycles
FOUND CAPT'S FLASHLIGHT INOP.
Part: LAMP — BURNED OUT (CABIN)
DURING A HANGAR INSPECTION, THE CEILING EMERGENCY LIGHT, ON THE AFT CEILING PANEL, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT, ON THE AFT CEILING PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2005
Part: STEP — BROKEN (PAX DOOR)
DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: STEP — CRACKED (PAX DOOR)
DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING A C-CHECK IN MCN, THE EMERGENCY CEILING LIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 17. OPERATIONAL CHECKS GOOD. (M)
2004
Part: BATTERY — INOPERATIVE (MEGAPHONE)
FLT 4696 - DURING A GROUND INSPECTION IN DFW, THE REAR PORTABLE MEGAPHONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE REAR PORTABLE MEGAPHONE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)
DURING AN A-CHECK IN BTR, THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE WIRES TO THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: FIXTURE — CORRODED (EMERGENCY LIGHT)
DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHT AT FS 690 WAS FOUND NOT TO ILLUMINATE. MAINTENANCE CLEANED CORROSION INHIBITOR FROM UNDER THE LAMP GROUND LUG. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: PROXIMITY SENSOR — MISALIGNED (MLG)
FLT 9950 - DURING CLIMB-OUT AFTER TAKEOFF FROM DFW-JFK, THE CREW SELECTED GEAR UP AND RECEIVED GEAR DISAGREE, NOSE STEERING INOPERATIVE AND WEIGHT ON WHEELS INPUT CAUTION MESSAGES. THE CREW COMPLIED WITH POH PROCEDURES AND DECLARED AND EMERGENCY. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE ADJUSTED BOTH NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSORS. OPS CHECKS GOOD. AIRCARFT OK FOR SERVICE. (M)
Part: ARM — DISCONNECTED (NLG)
FLT 4930 - DURING TAKEOFF FROM SNA-DFW, THE GEAR HANDLE WAS FOUND STUCK IN THE DOWN POSITION, FOLLOWED BY A SINGLE CHIME AND A WEIGHT ON WHEELS INPUT CAUTION MESSAGE. QRH PROCEDUES WERE COMPLEID WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED TO SNA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER NOSE LANDING GEAR NLG TORQUE ARM ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)