N147PQ
Registered owner: DELTA AIR LINES INC, GA (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.
191 reports on file, 2010-03-29 – 2026-07-21.
Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 41,148 hrs · 30,929 cycles
"DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED D (HINGE NR 2 OTBD) WAS PREVIOUSLY OVERSIZED. ENGINEERING IS REQUIRED. LUG D BORE MEASURES (0.8965). REPAIRED RT WING AILERON HINGE FITTING NR 2 OVERSIZED LUG BORES AT WS 319.604 IAW REO 690-57-51-549 REV --.
Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 41,148 hrs · 30,929 cycles
"DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED C (HINGE NR 2 INBD) WAS PREVIOUSLY OVERSIZED. ENGINEERING IS REQUIRED. LUG C BORE MEASURES (0.8985). REPAIRED RT WING AILERON HINGE FITTING NR 2 OVERSIZED LUG BORES AT WS 319.604 IAW REO 690-57-51-549 REV --.
Part: BUSHING — DAMAGED (ZONE 600 AILERON) · airframe 41,148 hrs · 30,929 cycles
RH AILERON 4 EACH BUSHING LUGS MARKED B, C, F AND G FOUND TO BE OVER SIZED UPON BUSHING REMOVAL. REPAIRED RH AILERON BUSHING LUGS B, C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.
Part: BUSHING — DAMAGED (ZONE 500 AILERON) · airframe 41,148 hrs · 30,929 cycles
LH AILERON FOUND 3 BUSHING LUGS MARKED C, F AND G TO BE OVER SIZED AFTER BUSHING REMOVAL REPAIRED LH AILERON BUSHING LUGS C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.
Part: LUG — DAMAGED (ZONE 500 AILERON) · airframe 41,148 hrs · 30,929 cycles
LH AILERON BEARING LUG MARKED E FOUND TO BE OVERSIZED UPON REMOVAL OF BEARING. RECEIVED MHIRJ REO 690-57-61-534 REV -- DATED 2026-07-11 COMPLIED WITH STEPS 1 REAM AND 2 CHAMFER IAW MHIRJ REO 690-57-61-534 REV -- DATED 2027-07-11 COMPLIED WITH STEP 1 REAM AND STEP 2 CHAMFER IAW MHIRJ REO 690-57-61-534 REV -- DATED 2026-07-11 PERFORMED EDDY CURRENT OF LH AILERON LUG BORE MARKED E IAW MHIRJ REO 690-57-61-534 REV -- DATED 2026-7-11 STEP 3 NO INDICATIONS NOTED AT THIS TIME COMPLIED WITH STEPS 4-8 IAW MHIRJ REO 690-57-61-534 REV -- DATED 2026-07-11 PN OF NEW BEARING IS KSC432409B-03
Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 41,148 hrs · 30,929 cycles
RH AILERON HAS 1 #9 BEARING LUG MARKED E FOUND TO BE OVER SIZED UPON BEARING REMOVAL. COMPLIED WITH STEPS 1 THRU 3 OF MHIRJ REO 690-57-61-273 REV-- DATED 2022-10-13. HFEC PERFORMED IAW MHIRJ REO 690-57-61-273 REV - DATED 2022-10-13 STEP 4 NO INDICATIONS NOTED AT THIS TIME COMPLIED WITH STEPS 5 THROUGH 10 IAW MHIRJ REO 690-57-61-273 REV -- DATED 2022-10-13BEARING P/N KSC432409B-01 REPLACEMENT IS COVERED UNDER LINE-ITEM 3A
Part: ANGLE — CORRODED (DOOR SILL) · airframe 41,148 hrs · 30,929 cycles
UPON REMOVAL FOUND LWR SILL ANGLE (P/N: SH670-31986-1) TO BE CORRODED AT UPPER FWD CORNER (BEYOND 90% MATERIAL MISSING) AND REQUIRE REPLACEMENT. REMOVED UNSERVICEABLE GALLY SERVICE DOOR LWR SILL ANGLE FROM MOUNTING ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED SERVICEABLE GALLY SERVICE DOOR LWR SILL ANGLE (P/N: SH670-31986-1) IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: DOOR — CRACKED (ZONE 800) · airframe 41,148 hrs · 30,929 cycles
R/H FWD OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED IAW MHIRJ REO 670-52-21-103, REV --, DATE 2024-11-06
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,148 hrs · 30,929 cycles
LEFT COCKPIT FLOORBEAM LBL12 AT BS 280 CRACKED. REINSTALLED BS 280 LT COCKPIT DOOR POST IAW SRM 51-42-06-001-001-A01, & SRM 51-42-13-001-001-A01. REMOVED SHORING FROM BS 250 BTWN S23L AND S23R IAW SRM 53-11-43-201-003-A01. INSTALLED NEW SERVICEABLE SEGMENT OF LT COCKPIT FLOORBEAM IAW SRM 53-11-43-201-003-A01, REPAIR TYPE IV. LOCATED & DRILLED NEW LBL 12 COCKPIT FLOORBEAM IAW SRM 51-40-11-001-001-A01. & SRM 53-11-43-201-003-A01. REPAIR TYPE 4.
Part: BRACKET — CRACKED (ZONE 800) · airframe 41,148 hrs · 30,929 cycles
RIGHT AFT OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED RT AFT OVERWING EMERGENCY EXIT DOOR UPPER BRACKETS IAW REO 670-52-21-103, REV --.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 41,148 hrs · 30,929 cycles
PAX DOOR INTERCOSTAL DD4 CORRODED. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR MID DD4 INTERCOSTAL. IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: BRACKET — CRACKED (ZONE 800) · airframe 41,148 hrs · 30,929 cycles
LEFT AFT OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED LT AFT OVERWING EMERGENCY EXIT DOOR UPPER BRACKETS IAW REO 670-52-21-103, REV -.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,148 hrs · 30,929 cycles
FS280 L/H CROSSBEAM HAS HEAVY PITTING CORROSION. REMOVED AND REPLACED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW LH FS 280.00 CROSSBEAM P/N:CC670-34094JP-1S IAW CRJ900 SRM 51-40-11-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,148 hrs · 30,929 cycles
FS280 R/H CROSSBEAM HAS HEAVY PITTING CORROSION. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. CRJ900 SRM 51-42-22-001-001-A01.
Part: DOOR — CRACKED (ZONE 800) · airframe 41,148 hrs · 30,929 cycles
LEFT FWD OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED THE LT FWD EMERGENCY EXIT IAW REO 670-52-21-103 REV -.
Part: ANGLE — CORRODED (ZONE 200) · airframe 41,148 hrs · 30,929 cycles
FS 280 FORWARD J-ANGLE IS CORRODED INSTALLED NEW J-ANGLE IAW SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW FS 280. J-ANGLE IAW SRM 51-40-11-001-001-A01.
Earlier reports · 2010–2022 · 175 reports
2022
Part: HOUSING — CHAFED (AFT CRGO DR HNDL) · airframe 33,343 hrs · 24,378 cycles
AFT CARGO DOOR HAS CHAFES AROUND OUTER HANDLE CUTOUT. REMOVED AND REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND AMM 52-31-03-400-801-A01.
Part: HOUSING — CHAFED · airframe 33,343 hrs · 24,378 cycles
AFT CARGO DOOR HAS CHAFES AROUND OUTER HANDLE CUTOUT. REMOVED AND REPLACED IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND CRJ 900 AMM 52-31-03-400-801-A01.
Part: FLOOR SUPPORT — CORRODED (BS 1026-1036) · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND OF FLOOR BEAM LBL9 BETWEEN FS 1026-1036. REPAIRED IAW CRJ-900 SRM 53-00-41-201-001-A03.
Part: ANGLE — CORRODED (BS 280 RBL 9) · airframe 33,343 hrs · 24,378 cycles
RBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280. FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: CONTACT — NONE · airframe 33,343 hrs · 24,378 cycles
"EMERGENCY LIGHT BELOW AFT L/H OVERWING EXIT DOOR IS INOP. " "FOUND BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY DS102 PIN #2, REQUIRES REPAIR. REPAIRED BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY BY CRIMPING SERVICEABLE CONTACT PN# B0808002-037 ONTO WIRE AND INSERTING INTO CONNECTOR IN ACCORDANCE WITH CRJ-900 ESPM 20-16-00. REPAIRED BROKEN WIRE ON PANEL 251NLW BY CRIMPING SERVICEABLE CONTACT PN# 350689-7 ONTO WIRE AND INSERTING INTO CONNECTOR IN ACCORDANCE WITH CRJ-900 ESPM 20-16-00. OPERATIONAL TEST OF EMERGENCY LIGHTS IS GOOD IN ACCORDANCE WITH CRJ-900 AMM 33-51-00-710-801-A01. WVAC EMP # 53517 "
Part: SKIN — CORRODED · airframe 33,343 hrs · 24,378 cycles
FUSELAGE INNER SKIN AT STGR 27 BETWEEN FS 677.00 AND 693.00 CORRODED. COMPLIED WITH REO 690-53-31-678 REV -- DATED 2022-10-14.
Part: INTERCOSTAL — CRACKED · airframe 33,343 hrs · 24,378 cycles
WHILE REPLACING SERVICE DOOR HANDLE FOUND INTERCOSTAL CRACKED REMOVED AND REPLACED INTERCOSTAL PN:CC670-38171-13 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,343 hrs · 24,378 cycles
INTERCOSTAL PN 601R31902-485 AT FS311-FS320 ON DATUM 6 OF PAX DOOR HAS CORROSION INSTALLED NEW INTERCOSTAL PN 601R31902-485 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: STIFFENER — CRACKED · airframe 33,343 hrs · 24,378 cycles
VERTICAL STIFFENER ON FWD PAX DOOR WEB IS CRACKED REMOVED CRACKED STIFFENER PN: 601R317742-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. AND INSTALLED NEW STIFFENER P/N 601R317742-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
Part: FRAME — CORRODED · airframe 33,343 hrs · 24,378 cycles
FRAME AT FS 661.00 BETWEEN STGR 17L AND 18L IS CORRODED. REPAIRED IAW REO NO 690-53-31-680 AND CRJ900 SRM 53-00-06-201-001-A03, FIG. 53-00-06-991-883.
Part: INTERCOSTAL — CORRODED · airframe 33,343 hrs · 24,378 cycles
INTERCOSTAL PN 601R31902-485 AT FS311-FS320 ON DATUM 6 OF PAX DOOR HAS CORROSION INSTALLED NEW INTERCOSTAL PN 601R31902-485 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: SKIN — CHAFED · airframe 33,343 hrs · 24,378 cycles
RH IB FLAP LOWER SKIN HAS CHAFING FROM CONTACT WITH IB FLAP FAIRING REPAIRED RIGHT HAND LOWER INBOARD FLAP IAW CRJ900 SRM 57-52-01-201-001-A01
Part: SEAT TRACK — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 INSTALLED NEW SEAT TRACK ON RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
Part: STRINGER — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON STGR 21R BETWEEN FS 409.00-485.00. INSTALLED STR21R PN SH670-31385-1S AND FS447.40 SPLICE PN SH670-33252-1 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: NONE — CORRODED · airframe 33,343 hrs · 24,378 cycles
RBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280 FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: FRAME — CRACKED · airframe 33,343 hrs · 24,378 cycles
FRAME AT FS 645.00 BETWEEN STGR 17L AND 18L IS CORRODED. REMOVED AND INSTALLED NEW SECTION FRAME AND SPLICE REPAIR ON FS645 BETWEEN STR16LH-STR18LH IAW REO NO 690-53-31-680 DATE 2022-10-14, AND SRM 53-00-06-201-001-A03, FIGURE 53-00-06-991-879, 51-42-06-001-001-A01.
Part: CLEAT — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON SUPPORT ANGLE AT FS 394.00 AT STGR 19L. REMOVED FABRICATED AND INSTALLED NEW STRINGER CLEAT @ FS. 394.00 STGR 19R IAW CRJ900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON STGR 19R BETWEEN FS295-310. REMOVED AND REPLACED STRINGER 19R FROM F.S 280-F.S 319 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: NONE — CORRODED · airframe 33,343 hrs · 24,378 cycles
LH FLOOR SILL BETWEEN FS 913.00 AND 969.00 IS CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED LH FLOOR SILL IAW CRJ900 SRM 51-42-06-001-001-A01 AND REO 690-53-51-350 REV-- DATED 2022-10-26
Part: FRAME — CRACKED · airframe 33,343 hrs · 24,378 cycles
L/H COCKPIT FRAME F.S.235 IS CRACKED. REPAIRED L/H COCKPIT FRAME FS 235 CRACK IAW MHIRJ REO 690-53-11-1474
Part: POST — CORRODED · airframe 33,343 hrs · 24,378 cycles
LBL 9 POST AT FS 280.00 IS CORRODED BETWEEN LH AFT WEB. REPAIRED LBL 9 POST FS 280.00 CORROSION ON LH AFT WEB PN CC670-34094JP1 AND JP2 IAW CRJ 900 SRM 53-11-10-201-004-A01
Part: STRINGER — CORRODED · airframe 33,343 hrs · 24,378 cycles
STRINGER 20R BETWEEN FS 597.00 AND 613.00 IS CORRODED. COMPLIED WITH STRINGER SPLICE REPAIR ON STRINGER 20R BETWEEN FS 597.00 AND FS 613.00 IAW CRJ-900 SRM 53-00-03-201-001-A02 REPAIR S6295 TYPE Z8 REPAIR.
Part: SEAT TRACK — CORRODED (BS 661-693 RBL9) · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 INSTALLED NEW SEAT TRACK ON RBL 9 BETWEEN F.S. 661+32-F.S. 693.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
Part: NONE — CORRODED · airframe 33,343 hrs · 24,378 cycles
LBL 9 ATTACHING CLIP TO "J" ANGLE CORRODED AT FS 280 FABRICATED AND INSTALLED J ANGLE ATTACHMENT CLIP ON RBL 9 TO 'J' ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: FRAME — CORRODED · airframe 33,343 hrs · 24,378 cycles
FRAME AT FS 927.00 IS CORRODED BETWEEN STGR 25R AND 26R. COMPLIED WITH SPLICE REPAIR OF FS 927.00 BETWEEN STGR 25R AND 26R IAW CRJ 900 SRM 53-00-06-201-001-A03.
Part: STRINGER — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON STGR 20R BETWEEN FS 364.00-379.00. REMOVED AND REPLACED NEW STRINGER P/N SH670-31405-2S AT FS 364 IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON STGR 26L BETWEEN FS 1015.00-1031.00 REPAIRED STGR 26L IAW MHIRJ REO 690-53-61-1126 REV. --, DATED 2022-10-24.
Part: BEAM — CORRODED · airframe 33,343 hrs · 24,378 cycles
TOP OF FLOOR BEAM AT RBL9 BETWEEN FS 693.00 AND 847.00 IS CORRODED IN MULTIPLE LOCATIONS. REPAIRED TOP OF FLOOR BEAM AT RBL 9 BETWEEN FS693.00 AND 847.00 CORROSION IAW MHIRJ REO 690-53-41-331 REV -- DATED 2022-10-21
Part: SEAT TRACK — CORRODED (BS 572-661) · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON RH SIDE SEAT TRACK BETWEEN FS 572.00-661+14. INSTALLED NEW SERVICEABLE RH SIDE SEAT TRACDK BETWEEN FS 572.00-661+14 IAW CRJ 900 SRM 53-00-49-400-801-A01
Part: SKIN — CORRODED (PAX DOOR) · airframe 33,343 hrs · 24,378 cycles
PASSENGER DOOR INNER SKIN CORRODED AROUND MULTIPLE NUTPLATE LOCATIONS. INSTALLED NEW INNER SKIN IAW SRM 51-42-06-001-001-A01,51-42-21-001-001-A01 AND 51-42-22-001-001-A01
Part: CLEAT — CORRODED · airframe 33,343 hrs · 24,378 cycles
CLEAT AT INTERSECTION OF FS320.16 AND DD6 IS CORRODED. REMOVED AND REPLACED CLEAT PN: 600-31902-269 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
Part: STIFFENER — CRACKED (PAX DOOR) · airframe 33,343 hrs · 24,378 cycles
PASSENGER DOOR AFT STAIR WEB STIFFENER, SECOND UP FROM THE LATCH END OF THE STAIR IS CRACKED. INSTALLED NEW STIFFENER PN:601R317747-1 IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: BRACKET — CRACKED · airframe 33,343 hrs · 24,378 cycles
FOUND PAX DOOR AFT HANDRAIL TO HAVE BROKEN SPRING BRACKET THAT KEEPS HANDRAIL LOCKED IN PLACE BROKEN. REMOVED AND REPLACE PAX DOOR AFT HANDRAIL SPRING BRACKET PN# 601R38587-19 PO# W 79466 IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-21-16-001-001-A01 A023.
Part: INTERCOSTAL — CORRODED (BS 311-320) · airframe 33,343 hrs · 24,378 cycles
INTERCOSTAL BETWEEN FS 311-320 ON DATUM 2 HAS CORROSION. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 483-572) · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON RH SIDE SEAT RAIL BETWEEN FS 483 TO F.S.572 REMOVED AND REPLACED RH SIDE SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.
Part: SKIN — CHAFED (RT WING) · airframe 33,343 hrs · 24,378 cycles
RIGHT WING PANEL 684JB HAS A CHAFE APPROX. 1.25 X 1.00 X .005 INCHES DEEP REMOVED AND REPLACED RH WING FLAP PANEL 684JB
Part: HINGE — CHAFED (PAX DOOR) · airframe 33,343 hrs · 24,378 cycles
PASSENGER DOOR HINGE FUSELAGE SIDE, AFT LUG LANDING IS CHAFED REMOVED AND REPLACED PASSENGER DOOR HINGE, FUSELAGE SIDE.
Part: SKIN — CHAFED (RT WING) · airframe 33,343 hrs · 24,378 cycles
RH WING LOWER SKIN IS CHAFED WHERE OB FLAP MID HINGE BOX FAIRING CONTACTED SKIN COMPLIED WITH MHRJ REO 690-57-21-426 REV-- DATED 2022-09-29.
Part: STRINGER — CRACKED (BS 280-295 S3L) · airframe 33,343 hrs · 24,378 cycles
FOUND FS280-295 STRINGER 3L HAS CRACK INDICATION NOTED IN MARKED FASTENER HOLES. REPAIRED STRG 3L F.S. 280-295 IAW BOMBARDIER REO 670-53-21-493 REV.-C DATED 2011/12/08
Part: SEAT TRACK — CORRODED (BS 581-661 RBL9) · airframe 33,343 hrs · 24,378 cycles
CORROSION FOUND ON SEAT TRACK RBL 9 BETWEEN F.S. 581.00- F.S. 661+32 INSTALLED NEW SERVICEABLE SIDE SEAT TRACK (PN: 20276-288-0-0A) IAW CRJ 900 AMM 53-00-49-400-801-A01
Part: WEB — CORRODED · airframe 33,343 hrs · 24,378 cycles
PASSENGER DOOR AFT WEB CRACKED AND CORRODED AT MULTIPLE LOCATIONS. INSTALLED NEW PAX DOOR AFT WEB P/N 601R317071-11 IAW CRJ 900 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
2021
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,854 hrs · 22,276 cycles
CABIN EMERGENCY LIGHTS DIM TO OFF WHEN TURNED ON. - REMOVED AND REPLACED ALL 5 EPSU BATT. PACKS IAW CRJ900 AMM 33-51-17. OPS CHECK GOOD.
2020
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,161 hrs · 20,741 cycles
REAR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EPSU BATTERY PACK PS38 IAW AMM 33-51-17, OPS CHECK GOOD P/N ON AD-2013-1A, P/N OFF 2013-1ASMI, S/N ON 135762 S/N OFF 7399.
Part: RETAINER — BENT (PAX DOOR) · airframe 28,753 hrs · 20,406 cycles
BENT ON BOTTOM PRESSURE SEAL RETAINER OF PASSENGER DOOR."SUMMARY: BOTTOM PRESSURE SEAL RETAINER OF PASSENGER DOOR WAS REPLACEDFOR NEW ONE PER CRJ 900 SRM 51-42-10. "
Part: RETAINER — WORN (CARGO DOOR) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: BENT AND WEAR ON LOWER PRESSURE SEAL RETAINER IN FWD/AFT CORNER AT FWD/CENTER BAGGAGE BAY DOOR.(CCD.) "SUMMARY: LOWER PRESSURE SEAL RETAINER IN FWD/AFT CORNER AT FWD/CENTERBAGGAGE BAY WERE REPLACED PER CRJ-900 SRM 51-42-21. "
Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STRG 26L-26R AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "INTERCOSTALS (4EAS) BTW FS 349-364, STRG 26L-26R WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. CORROSION LEVEL: 2
Part: DOOR SILL — CORRODED · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE (FUS) (TCI 53-20-220) ""LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. CORROSION LEVEL 2 "
Part: FLOOR SUPPORT — CRACKED (BS 270-280) · airframe 28,753 hrs · 20,406 cycles
"AWR. CRACK ON FLOOR BEAM LBL 12 BTW FS 270-280 AT FLIGHT COMPARTMENT ""FLOOR BEAM LBL 12 BTW FS 270-280 AT FLIGHT COMPARTMENT WAS REPAIRED PER CRJ-900 SRM. 53-11-43-201-003-A01 "
Part: CARGO TRACK — WORN (CARGO BAY) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: WEAR FLOOR TRACK PN: 500171 OF CARGO RETRIEVAL SYSTEM SIDE GUIDE AT FWD BAGGAGE BAY (C1) "TRACK OF CARGO RETRIEVAL SYSTEM SIDE GUIDE WAS REPLACED FOR A NEW ONEPER CRJ900 AMM 25-51-02 "
Part: SUPPORT FITTING — CORRODED · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON FWD JACK FITTING LH SUPPORT ATFWD AVIONICS COMPARTMENT.(SM)(E/E)(TCI 53-10-305) "||CORROSION LEVEL 2|| FWD JACK FITTING LH SUPPORT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01
Part: FITTING — CORRODED (NLG DOOR) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"AWR AFTER AFT NLG DOOR AIRFRAME BUSHINGS REMOVAL, CORROSION WAS FOUNDON FRAME HINGE LH/RH FITTINGS AT NLG WHEEL WELL. "CORROSION LEVEL 2: FRAME HINGE LH/RH FITTINGS AT NLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 "
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 684HT, 684FT, 684ET, 584HTAND 584ET. (AI)(AD). "ACCESS PANEL 684ET WAS REPAIRED PER EA CRJ957-10144 REV. ""IR"", 684HT REPAIRED PER EA CRJ957-10139 REV. ""IR"", 584HT REPAIRED PER EA CRJ657-10143 REV. ""IR"", 684FT WAS REPAIRED PER EA CRJ957-10140 REV. ""IR"",. 584ET WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-01.
Part: RETAINER — BENT (TE FLAP HINGE) · airframe 28,753 hrs · 20,406 cycles
"PART RACKS: BENT ON SEAL RETAINER OF FLAP HINGE FAIRING LH WING NBR 597BB OUTBD SIDE.(SM)(AI) ""AFT HINGE FAIRING ASSY P/N:CC670-17900-1 WAS REPLACED FOR SERVICEABLE AND VERIFIED PER CRJ900 AIPC 57-51-84-20. FIG.20 ITEM 40, THEREFORE DISCREPANCY (BENT ON SEAL RETAINER) WAS CORRECTED AND FAIRING 597BB WAS INSTALLED PER CRJ900 AMM 57-51-84-400-805 A01 "
Part: SKIN — CORRODED (L1 DOOR) · airframe 28,753 hrs · 20,406 cycles
"AWR IN REF NRC NBR 00195, FWD SIDE PANELS SKIN AT PASSENGER DOOR (L1).ITS OUT OF LIMITS ""FWD SIDE PANEL SKIN AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 CORROSION LEVEL 2
Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON FRAME FS 319, STRG 25L-25R AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "FRAME FS 319, STRG 25L-25R, WAS REPAIRED PER EA NO: CRJ953-10198 REV IR. (LEVEL CORROSION 2) "
Part: BRACKET — CORRODED (DOOR FRAME) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON SENSOR(PX36) BRACKET AT SERVICE DOOR SURROUND STRUCTURE. (TCI 53-20-320) ""BRACKET WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01. (CORROSIONLEVEL 2) "
Part: ANGLE — CORRODED (PAX DOOR FRAME) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE (W1)"ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED FOR ANEW ONE PER CRJ-900 SRM 51-41-02-001-001-A01 (LEVEL CORROSION 2) "
Part: STRAP — CORRODED (WING TO BODY) · airframe 28,753 hrs · 20,406 cycles
"PART RACK. CORROSION ON FITTING STRAPS (2EAS) OF WING TO FUSELAGE PANEL 193AB. "FITTING STRAPS (2EA) OF WING TO FUSELAGE PANEL 193AB WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 ( LEVEL CORROSION 2) "
Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON LOWER STRIKER AT SERVICE DOOR SURROUND STRUCTURE. (TCI 53-20-320) "LOWER STRIKER AT SERVICE DOOR SURROUND STRUCTURE WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND STOP FITTINGS WAS INSTALLED PER NRC 00490. LEVEL CORROSION: 2. "
Part: WEB — CRACKED · airframe 28,753 hrs · 20,406 cycles
INITIAL INSPECTION: CRACK ON WEB BELOW OF ADG RESTOW PUMP. (S/M])(CAD) "WEB BELOW OF ADG RESTOW PUMP WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01. "
Part: STRINGER — CORRODED (BS 280-379) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRINGER R23 BTW FS 319-349 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "STRINGER 23RH BTW FS 280 TO FS 379 WAS REPLACED PER CRJ-900 SRM-51-42-06-001-001-A01 (LEVEL CORROSION 2). "
Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF NRC S/N 00274, CORROSION DAMAGE OUT OF LIMITS ON INTERCOSTAL STRG R20 BTW FS 310-319 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). ""INTERCOSTAL STRG R20 BTW FS 310-319 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. LEVEL CORROSION: 2 "
Part: STRINGER — CORRODED (BS 310-379) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRINGER R21 BTW FS 310-349 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "SECTION STRINGER R21 BTW FS 310 TO FS333 WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND NO DISCREPANCIES WERE NOTED AND STRINGER 21 RH SECTION FS333 TO FS379 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEVEL CORROSION: 2 "
Part: STRINGER — CORRODED (BS 280-333) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRINGER R22 BTW FS 319-349 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "STRINGER 22RH SECTION FS280 TO FS333 AND SECTION FS333 TO FS349 WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEVEL CORROSION: 2 "
Part: STRINGER — CORRODED (BS 333-349) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRINGER R22 BTW FS 319-349 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "STRINGER 22RH SECTION FS280 TO FS333 AND SECTION FS333 TO FS349 WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEVEL CORROSION: 2 "
Part: ACCESS PANEL — CRACKED · airframe 28,753 hrs · 20,406 cycles
"HIDDEN DAMAGE :IN REF NRC S/N 00421, DURING STIFFENER REMOVAL,CRACK ON ACCESS 171CL WAS FOUND. (FUS)(SM). "CRACK ON ACCESS 171CL WAS REPAIRED PER REO 670-53-82-430 REV --
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD). "ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001-001-A01.
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD). " "ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001-001-A01. "
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD). ""ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001-001-A01.
Part: DOUBLER — CORRODED (BS 295-310) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON INTERNAL DOBLER BTW FS 295-310 STRG 26L-26R AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "INTERNAL DOUBLER WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01. LEVEL CORROSION: 2 "
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD). "ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001-001-A01. " "
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 28,753 hrs · 20,406 cycles
"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD). ""ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001-001-A01. " CC670-14179-1
Part: STRUCTURE — CORRODED (BS 349) · airframe 28,753 hrs · 20,406 cycles
"AWR. CORROSION ON PACKER FS 349-RBL 9 BTW LONGITUDINAL BEAM AND CROSS BEAM. "PACKER WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-21-001-001-A01. LEVEL CORROSION: 1 "
Part: TUBE — CORRODED (PAX DOOR FRAME) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON TUBE AT PASSENGER DOOR SURROUND STRUCTURE (FUS) "TUBE WAS REPLACED FOR A NEW ONE PER CRJ-900 AMM 52-11-00-400-802-A01.LEVEL CORROSION: 1
Part: CHANNEL — CRACKED · airframe 28,753 hrs · 20,406 cycles
"EDV AIR: PANEL 196DR CHANNEL CRACKED REPLACE WITH NEW CC690-39251-1 CHANNEL. (FUS). "CHANNEL WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-10-001-001-A01. "
Part: STRINGER — CORRODED (BS 333-364) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON STRINGERS 26R AND 26L BTW FS 333-364 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "STRINGERS 26R AND 26L BTW FS 333-364 AT MAIN AVIONICS COMPARTMENT WERE REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 CORROSION LEVEL 2 "SH670-31372-3S
Part: STRINGER — CORRODED (BS 280-333) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON STRINGER SPLICE 25R BTW FS 333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "CORROSION ON STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 "
Part: STIFFENER — CRACKED · airframe 28,753 hrs · 20,406 cycles
POST-PART RACKS: CRACKED STIFFENER ON ACCESS PANEL 171CL (FUS)(SM) "STIFFENER ON ACCESS PANEL 171CL WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01. "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,753 hrs · 20,406 cycles
"CORROSION ON FLOOR SUPPORT FS 280 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "SUMMARY: FLOOR SUPPORT FS 280 AT MAIN AVIONICS COMPARTMENT T WAS FOUND WITH MORE THAN 50% OF THE DAMAGES ALLOWED, THEREFORE ITS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. EQUIPMENT DIAL INDICATOR P/N: 543-783 SERIA NO. 18200766 DUE DATE: 19/MAR/2020.FLOOR SUPPORT WAS REPLACED FOR FOR A NEW ONES P/N CC670-34256-3 PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
Part: STRINGER — CORRODED (BS 280-333) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09)."STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 CORROSION LEVEL 2
Part: STRINGER — CORRODED (BS 280-333) · airframe 28,753 hrs · 20,406 cycles
"AWR, HIDDEN DAMAGE [DURING PERFORMING OF NRC 00274]: CORROSION ON STGR 20R BTW FS310-319.70 WAS FOUND. (FUS). ""STRINGER 20RH BTW FS280 TO FS333 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-20-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01.LEVEL CORROSION: 2 "
Part: ANGLE — CORRODED (SERVICE PANEL) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON IMPACT ANGLE, UPPER/LOWER DIAPHRAGM, UPPER/LOWER AFT ANGLE AND PLATE OF FWD WATER WASTE SERVICE PANEL. (SM)(FUS)(TCI 100-16). "CORROSION WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND REWORKED AREAS ON UPPER/LOWER DIAPHRAGM, UPPER/LOWER AFT ANGLE AND PLATE OF FWD WATER WASTE SERVICE PANEL WERE MEASURED WITH THE FOLLOWING DIMENSIONS: UPPER/LOWER DIAPHRAGM, OT=0.080"" MRT= 0.078"" MAX DEPTH= 0.002"", UPPER/LOWER AFT ANGLE: OT=0.063"" MRT= 0.061"" MAX DEPTH= 0.002"" AND PLATE : OT=0.157"" RT= 0.155"" MAX DEPTH= 0.002"" THEREFORE IT'S WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101001A01 AND IMPACT ANGLE WAS REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01. LEVEL CORROSION 1
Part: FLOORBEAM — CORRODED (BS 314) · airframe 28,753 hrs · 20,406 cycles
"AWR, IN REF NRC S/N 00236, AFTER ANGLE REMOVAL, CORROSION WAS FOUND ON FLOOR SUPPORTS AT PASSENGER SURROUND AREA LOWER SILL. "FWD FLOOR SUPPORT STA 314 AT PASSENGER SURROUND AREA LOWER SILL WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND CORROSION ON AFT FLOOR SUPPORT AT PASSENGER SURROUND AREA LOWER SILL WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 BLENDED AREA WAS MEASURE AND FOUND WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02. LEVEL CORROSION: 1
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF NRC S/N 00274, CORROSION DAMAGE OUT OF LIMITS ON INTERCOSTAL STRG R20 BTW FS 349-364 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). ""INTERCOSTAL STRG R20 BTW FS 349-364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001-A01. LEVEL CORROSION: 2 "
Part: INTERCOSTAL — CORRODED (BS 310-349) · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON INTERCOSTAL STRG L21 BTW FS 310-349 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "CORROSION LEVEL 2 INTERCOSTAL STRG L21 BTW FS 310-333 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6C AND CRJ-900 SRM 51-42-20-001-001-A01 PAR 6C AND CORROSION ON INTERCOSTAL STRG L21 BTW FS 333-349 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR 5B, B
Part: STRINGER SPLICE — CORRODED (BS 333) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRIGER SPLICE R21, R22, R23- FS 333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09). "STRINGER SPLICE R21, R22, R23- FS333 AT MAIN AVIONICS COMPARTMENT WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEVEL CORROSION: 2 "
Part: COAMING — WORN (LT NACELLE) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: WEAR ON CUT OUT (COAMING) OF LATCH DOOR AT LH ENGINE UPPER TRANSCOWL. (MOT1). ""COAMING WAS REPLACED FOR NEW ONE (P/N: CN624-2060-209) PER CRJ900 SRM51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01. "
Part: SUPPORT PLATE — CORRODED (FLOOR) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: CORROSION ON PLATE PROTECTOR SUPPORTS (4EAS) AT SERVICE DOOR SURROUND STRUCTURE. (TCI 53-20-320) "PROTECTORS WEB FLOOR (4EAS) WERE REPLACED FOR NEW ONES PER CRJ900 SRM51-42-21-001-001-A01 PAR 6C. LEVEL CORROSION:1 "
Part: STRIKER — WORN (PAX DOOR FRAME) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: WEAR ON LOWER STRIKER AT PASSENGER DOOR SURROUND STRUCTURE (W1) "LOWER SEAL STRIKER WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-21-001-001-A01 PAR.6.C AND SRM 51-42-06-001-001-A01 PAR.6.C. "
Part: SPIGOT — WORN (NACELLE DOOR) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: WEAR ON SPIGOT AT TRANSCOWL LATCH DOOR LH ENGINE.(MOT1) ""SPIGOT AT TRANSCOWL LATCH DOOR LH ENGINE WAS REPLACED FOR NEW ONE (P/N: CN624-2067-205) PER CRJ-900 SRM 51-42-06-001-001-A01. "
Part: DRAIN PAN — CORRODED (BS 280) · corrosion level 2 · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION. CORROSION ON LH DRAIN PAN OF FS 280 CROSS BEAM LBL 19. (TCI 53-10-219). "SUMMARY OF NRC 00176 CORROSION LEVEL-2 : L/H DRAIN PAN OF FS 280 CROSS BEAM LBL 19. WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-#01 "
Part: LATCH — WORN (NACELLE DOOR) · airframe 28,753 hrs · 20,406 cycles
"INITIAL INSPECTION: WEAR ON SETTLEMENT AREA OF DOORS 444CT AND 444CB (ON STRUCTURE OF FWD CORE-COWL) RH ENGINE RH-MOT-2 ""SUMMARY: REINFORCING LATCH ON ACCES DOORS 444CT AND 444CB WERE REPLACED FOR NEW ONE (2E/A, P/N:CN624-3084-201) PER CRJ900 SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01. "
2018
Part: OXYGEN BOX — DAMAGED (COCKPIT) · airframe 25,121 hrs · 17,691 cycles
PILOT OXYGEN MASK BOX DAMAGED. REMOVED AND REPLACED THE OXYGNE MASK BOX IAW AMM 35-11-15.
2016
Part: DIMMER — DEFECTIVE (COCKPIT) · airframe 21,585 hrs · 15,119 cycles
PILOT REPORTS FLT LEVEL 240 GOT VERY STRONG SMELL THAT SMELLED LIKE ELECTRICAL FIRE, BUT NO SMOKE. DECIDED TO DIVERT TO YYZ. MTC REMOVED AND REPLACED LAMP DRIVER UNIT IAW AMM 31-41-07, IPC REF 31-41-07 FIG 1, ITEM 5. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 21,296 hrs · 14,923 cycles
EMERGENCY EXIT ROW SIGNS KEEP FLICKERING AT ROW 12. REPLACED THE BATTERY PACK. LIGHTS OPS CHECKED GOOD IAW AMM 33-51-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,291 hrs · 14,918 cycles
FLIGHT CREW REPORTED, EMERGENCY EXIT ROW SIGNS, BOTH SIDES, KEEP FLICKERING AT ROW 12 CENTER CEILING LIGHT, AFT LIGHT ASSY AND BOTH LT AND RT LOWER EXIT SIGNS FLICKER WHEN OFF AND DO NOT COME ON WHEN SELECTED ON. MX REPLACED EMERGENCY BATTERY AT ROW 10 OVERHEAD, P5452, AND ALL LIGHTS OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE IAW AMM 33-51-00.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDE SEAT TRACK AT BS 661+16 - 661+90 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801-A07, AND SRM 53-00-49-400-801-A07.
Part: STRAP — CORRODED (BS 319) · airframe 21,199 hrs · 14,852 cycles
SERVICE DOOR SURROUND LOWER FWD OUTER STRAP CORRODED AT BS 319.70. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, AND FOUND OUT OF LIMITS IAW SRM 53-21-23-101-001-A02. REMOVED AND REPLACED THE STRAP IAW SRM 51-42-21-001-001-A01, SRM 51-21-06-001-001-A01 AND DRAWING SH670-31950.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK LBL 9 BS 581 - 661+32 HAS CORROSION. BLENDED AND FOUND OUT OF LIMITS IAW AMM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 813) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDEWALL SEAT TRACK AND DADO PANEL SUPPORT HAS CORROSION AT BS 813.70. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
RIGHT SIDEWALL SEAT RAIL AND DADO SUPPORT HAS CORROSION AT FS 785.15. DAMAGE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED SUPPORT BY REMOVING SEAT RAIL IAW AMM 53-00-49-000-801-A07 THEN PULLING FROM STRUCTURE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. RECEIVED REPAIR STS EA 252016-203. COMPLIED WITH STS EA 25-2016-203. INSTALLED RT SIDE WALL SEAT RAIL DADO SUPPORT IAW AMM 53-00-49-400-801-A07.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDEWALL SEAT RAIL AND DADO SUPPORT HAS CORROSION AT FS 720.85. LT SIDEWALL SEAT RAIL AT FS 720.85 WILL BE REPLACED ON JOB 71514748, OP 14 DADO SUPPORT OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED CORROSION FROM SUPPORT IAW RM 51-21-06-001-001-A01. RECEIVED EA 25-2016-204 AND REPAIRED LT SIDEWALL DADO SUPPORT IAW STS EA 25-2016-204. INSTALLED LT SIDEWALL SEAT RAIL DADO SUPPORT AT FS 720.85 IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDE SEAT TRACK BS 661+16 - 661+74 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDE SEAT TRACK BS 565 - 661+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND SRM 53-00-49-400-801-A01.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK RBL 9 BS 581 - 661+32 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-807, AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK RBL 9 BS 349 - 485 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 643-830) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK LBL 9, BS 643-830.40 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 21,199 hrs · 14,852 cycles
DEFECT DESCRIPTION: RH SIDE SEAT RAIL FS661-16 - 661+90 HAS CORROSION. FOUND TO BE OUT OF LIMITS PER SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A01, AND 53-00-49-400-801-A01.
Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK RBL 9 BS 693 - 830 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-01-101-001 A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07, AND AMM 53-00-41-400-801 A01.
Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 21,199 hrs · 14,852 cycles
RIGHT SIDE SEAT TRACK BS 565 - 661+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS PER SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDEWALL SEAT TRACK SEGMENT BS 785.15 - 847+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-14-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 21,199 hrs · 14,852 cycles
RIGHT SIDE WALL SEAT TRACK SEGMENT BS 669.10 - 720.85 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK RBL 9 BS 661+32 - 693 HAS CORROSION. FOUNDTO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 21,199 hrs · 14,852 cycles
LEFT SIDE SEAT TRACK BS 485 - 565 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 21,199 hrs · 14,852 cycles
SEAT TRACK LBL 9 BS 661+32 - 693 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
CARGO FLOORBEAM HAS CORROSION AT LBL9 AT FS1031. REMOVED CORROSION ON LBL9 AT FS 1031 IAW SRM 51-21-06-00-0001-A01. FOUND TO BE OUT OF LIMITS DUE TO 50 PERCENT MATERIAL LOSS WHERE NO DAMAGE IS ALLOWED. COMPLIED WITH EO 900-53-0029 IAW GREO 670-53-00-029, REV A.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
CARGO FLOORBEAM HAS CORROSION AT LBL27, FS1010-1031. REMOVED CORROSION ON LBL27 AT FS1010-1031 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43-201-001-A02. COMPLIED WITH EO 900-53-0030 IAW FREO 670-53-00-029, REV A.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
FLOOR SUPPORT ANGLE AT THE SERVICE DOOR CORRODED. SUPPORT ANGLE BEYOND LIMITS IAW SRM 53-21-23-101-001, A02 ANGLE NEEDS TO BE REPLACED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06-001-001 A01 AND DWG SH670-3186. ASSEMBLED SUPPORT ANGLE AND PROTECTOR ANGLE ASSY IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. INSTALLED FLOOR SUPPORT ANGLE ASSY IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
CORROSION ON FLOOR SILL FWD OF SERVICE DOOR AT FS 310.00. REMOVED CORROSION ON RT FLOOR SILL AT FS 349.00 IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS OF GREO. COMPLIED WITH REO 690-53-21-609, REV A. RECEIVED & COMPLIED WITH EC/TC REO 690-53-21-609.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
RT SIDE SEAT TRACK CORRODED AT FS 752.50. RT SIDE SEAT TRACK FS 752.50 IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. COMPLIED WITH EC/TC REO 670-53-00-363 ANDG REO 670-53-00-353 REV.M. REMOVED RT SIDE SEAT TRACKS AT FS 752.50 IAW AMM 53-00-49-000-801-A01. INSTALLED RT SIDE SEAT TRACK AT FS 752.50 IAW SRM 53-00-49-400-801-A01.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
CORROSION ON FLOOR SILL AFT OF SERVICE DOOR AT FS 349.00. REMOVED CORROSION ON RT FLOOR SILL AT FS 349.00 IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS OF GREO. COMPLIED WITH REO 690-53-21-609, REV A, RECEIVED AND COMPLIED WITH EC/TC REO 690-53-21-609.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
CORROSION SERVICE DOOR FLOOR SILL. LOWER ANGLE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-23-101-001-A02, REPLACE WHEN PAT RECEIVED. REMOVED LOWER ANGLE IAW SRM 51-42-06 AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01 AND DWG SH670-31950. INSTALL SERVICE DOOR FLOOR SILL ANGLE IAW SRM NEW 57-42-06-001-001-A01 AND DWG SH670-31950.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
RT SIDE SEAT TRACK CORRODED NR FS 785.15 DAMAGE OUT OF LIMITS IAW SRM 53-31-49-101-001-A02. COMPLELED REMOVAL AT RT SIDE SEAT TRACK AT FS 785 IAW CRJ900 AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 REV M. INSALLED RT SIDE SEAT TRACK AT FS 785.15 IAW AMM 53-00-49-000-801.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
SIDE SEAT TRACK AT FS 752.50 LT SIDE CORRODED. LT SIDE SEAT RAIL FS 752.50 IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. COMPLIED WITH EC/TC REO 670-53-00-363 AND GREO 670-53-00-353, REV M. REMOVED LT SIDE SEAT RAIL FS 744-752.50 IAW SRM 53-00-49-000-801-A07. INSTALLED LT SIDE SEAT RAIL FS 744-753.50 IAW SRM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
LT SIDE SEAT TRACK AT FS 720.85 CORRODED. LT SIDE SEAT TRACK FS 720.85 CORRODED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02. REMOVED LT SIDE SEAT TRACK AT FS 728385 IAW AMM 53-00-9-000-801-A07. FABRICATED AND INSTALLED SEAT RAIL AT FS 720.85 LT SIDE. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M. INSTALLED LT SIDE SEAT TRACK AT FS 720.85 IAW AMM 53-00-49-400-801.
Part: HINGE — GOUGED (PAX DOOR) · airframe 21,199 hrs · 14,852 cycles
PASSENGER DOOR HINGE LUGS NR 1, NR 6, NR 11,NR 27, DOOR SIDE, ARE GOUGED, COUNTING FROM FRONT TO BACK. REPAIRED PASSENGER DOOR HINGE, DOOR SIDE IAW ECTC REO 670-52-11-511 AND REO 670-52-11-511, REV A AS WRITTEN.
Part: RETAINER — DAMAGED (PAX DOOR) · airframe 21,199 hrs · 14,852 cycles
DURING DAMAGE EVALUATION, IT WAS DISCOVER THAT THE PASSENGER DOOR OUTER SKIN, UPPER SURFACE WAS DENTED, FS 317.00 TO FS 323.00. COMPLIED ECTC/EA 20-2016-230. REMOVED UPPER SEAL RETAINER DUE TO DAMAGE TO IT IAW SRM 51-42-06-001-001-A01, BUCKLED. INSTALLED UPPER SEAL RETAINER TO PASSENGER DOOR IAW SRM 51-42-06-001-001-A01. LOCATED & DRILLED NEW SERVICEABLE UPPER SEAL RETAINER IAW SRM 51-40-11-001-001-A01 & 51-40-06-001-001-A01 & DWG 601R31702. REMOVED TOP SEAL RETAINER DUE TO DAMAGE IAW SRM 51-42-06-001-001-A01, BLENDED & BENT. INSTALLED NEW TOP SEAL RETAINER IAW SRM 51-42-06-001-001-A01. LOCATED & DRILLED DEBURRED TOPS EAL RETAINER IAW SRM 51-40-11-001-001-A01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
FS 333.00, FRAME HAS CORROSION BETWEEN STR 27R-26R. REMOVED CORROSION AT FS 333, FRAME AND BETWEEN STR 27-26R IAW SRM 51-21-06-001-001 A01. DAMAGE IS OUT OF LIMITS IAW SRM 53-21-06-101-006, A02. COMPLIED WITH EA 26-2016-208, REV P1. RECEIVED AND COMPLIED WITH EA 26-2016-208.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
INTERCOSTAL AT STR 27R HAS CORROSION BETWEEN FS 349.00 AND FS 364.00. R & R INTERCOSTAL AT STR 27R BETWEEN FS 349.00 AND FS 364.00 REF SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-32050, REV J.
Part: FRAME — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
FS 295, FRAME HAS CORROSION BETWEEN STR 27-24R. REMOVED CORROSION AT FS 295 FRAME AT STR 24R. THE CORROSION & FS 295 BETWEEN STR 27 AND 25R OUT OF LIMITS. FRAME 295, MATERIAL LOSS AT STR 24R IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-101-001-A01. DAMAGE AT STR 25R-27R IS REPAIRED IAW GREO 670-53-21-799. DAMAGE FROM STR 25R TO STR 24R IS WITHIN LIMITS IAW SRM 53-00-00-101-001-A01. DAMAGE 26L TO 25R IS OUT OF LIMITS. REPAIRED FRAME STA 295 IAW REO 670-53-21-799.
Part: STRAP — CORRODED (FUSELAGE) · airframe 21,199 hrs · 14,852 cycles
FS 280 BUTT STRAP HAS CORROSION FROM STR 26L-24R. REMOVED CORROSION IN DISCREPANT AREAS REF: SRM 51-21-06-001-001-A01. REPLACED AFFECTED FASTENERS IN FS 280 BUTT STRAP BETWEEN STR 26L & 24R, REF SRM 51-42-06-001-001-A01. COMPLIED WITH EC/TC EA 20-2016-244, REV O, DATED 8/5/2016.
2015
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 18,882 hrs · 13,176 cycles
RIGHT EXTERNAL REAR FUSELAGE EMERGENCY LIGHT LENS COVER BROKEN. R & R RT EXTERNAL EMERGENCY LENS IAW AMM 33-51-15.
2014
Part: RETAINER — TORN (CARGO BAY) · airframe 16,683 hrs · 11,685 cycles
FWD CARGO FWD DOOR SEAL RETAINER RIPPED AT LOWER FWD CORNER. COMPLIED WITH EC/TC REO 690-52-35-013. MAJOR REPAIR IAW GMM 5-3.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,234 hrs · 10,722 cycles
UPPER EMERGENCY LIGHT AT PAX DOOR ON F/A'S STATION DOES NOT WORK. R & R FIVE LAMPS IAW AMM 33-57-00-710-802, OPS TESTED GOOD.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 15,234 hrs · 10,722 cycles
BOTH LT FWD OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. SECURED CONNECTIONS FOR BOTH LIGHTS DS97 AND DS99 THEN COMPLIED WITH OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-802. OPS TEST GOOD.
Part: SIDEWALL PANEL — DAMAGED · airframe 15,234 hrs · 10,722 cycles
PAX DOOR, FWD AND AFT SIDEWALL DAMAGED. INSTALLED PERMANENT REPAIR IAW REO 690-52-11-285.
Part: BRACKET — CRACKED (BS 280) · airframe 15,225 hrs · 10,716 cycles
FWD SIDE OF BS 280 BEAM LIGHT BRACKET IS CRACKED AND LIGHT ASSY IS BROKEN. REMOVED & INSTALLED NEW SERVICEABLE LIGHT BRACKET IAW SRM 51-42-06-001-001 & DWG CC 670-51620. INSTALLED SERVICEABLE FWD AVIONICS LIGHT ASSY IAW AMM 33-32-01-400-801. OPS TEST GOOD.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 15,225 hrs · 10,716 cycles
FLOORBEAM IN COCKPIT IS CRACKED. REPAIRED IAW REO 690-53-11-630, REV A. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 15,225 hrs · 10,716 cycles
FLOORBEAM IN COCKPIT IS CRACKED. REPAIRED IAW REO 690-53-11-630. MAJOR REPAIR.
Part: NUT PLATE — MISSING (FLOOR PANEL) · airframe 15,225 hrs · 10,716 cycles
FWD CARGO FLOOR PANEL 151TLW MISSING NUTPLATE. REPLACED MISSING NUTPLATE IAW SRM 51-42-15-001-001. MAJOR REPAIR.
Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 15,225 hrs · 10,716 cycles
FUSELAGE TO VERTICAL ATTACH POINT LT DRAG ANGLE CRACKED AT FRAME 67. REPAIRED LT DRAG ANGLE IAW REO 690-55-31-004. MAJOR REPAIR.
Part: SKIN — DAMAGED (BS 927) · airframe 15,225 hrs · 10,716 cycles
SKIN DAMAGED AT STRINGER 27 BS 927. COMPLIED WITH EC/TC REO 670-53-00-290 AND EC/TC MODSUM IS67053820002. BLENDED OUT DAMAGE ON SKIN BS 913-927.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,225 hrs · 10,716 cycles
BS 280 FLOORBEAM CORRODED. REMOVED FLOORBEAM IAW 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01. INSTALLED FLOORBEAM IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,223 hrs · 10,715 cycles
BS 280 FLOORBEAM CORRODED. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLE FLOORBEAM IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,225 hrs · 10,716 cycles
INTERCOSTAL CORRODED BETWEEN BS 349 & 364 S27L. REMOVED INTERCOASTAL IAW SRM 51-12-06 AND SRM 51-42-20. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-46-11. INSTALLED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32050.
Part: FRAME — CORRODED (BS 333) · airframe 15,225 hrs · 10,716 cycles
FRAME BS 333 CORRODED BETWEEN S25 - 27R. REMOVED CORROSION IAW SRM 53-21-06-101-006-A02. COMPLIED WITH FWD 690-53-21608.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,225 hrs · 10,716 cycles
INTERCOSTAL CORRODED BETWEEN BS 349 & 364 S27L. R & R INTERCOSTAL. IAW SRM 51-42-06-001-001-A01, DWG SH670-32075 AND 51-42-21-001-001-A01, SRM 51-42-06 AND DWG SH670-32075.
Part: STRINGER — CORRODED (BS 333-349) · airframe 15,225 hrs · 10,716 cycles
STRINGER 26R CORRODED BETWEEN BS 333 & 349. REMOVED CORROSION IAW SRM 53-21-03-101-006-A02. FOUND TO BE SATISFACTORY.
Part: STRINGER — CORRODED (BS 319-333) · airframe 15,225 hrs · 10,716 cycles
STRINGER 26R CORRODED BETWEEN BS 319.7 & 333. REMOVED STRINGER BETWEEN BS 280 --333 IAW SRM 51-42-06-001-001-A01, 51-424-21-001-001-A01. INSTALLED STRINGER IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (BS 295) · airframe 15,223 hrs · 10,715 cycles
ANGLE CRACKED AT FLOORBEAM FS 295, LBL 9. R & R ANGLE ON FLOORBEAM IAW SRM 51-42-21-001-001-A01 AND DWG SH670-36236.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 15,225 hrs · 10,716 cycles
RT FLOOR SUPPORT CORRODED AT BS 349. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND TEMP REV 51-0050 AND REO 670-53-00-390.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,225 hrs · 10,716 cycles
COCKPIT FLOORBEAM BS 280 CORRODED. REMOVED FLOORBEAM ANGLE FS 280, WL 73, LBL 11 - RBL 11 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. MAJOR REPAIR.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,225 hrs · 10,716 cycles
INTERCOSTAL CORRODED BETWEEN BS 349 & 364, S26R. REMOVED INTERCOSTAL IAW SRM 51-42-06, TASK 51-42-06-001-001-A01. INSTALLED INTERCOSTAL IAW SRM 51-42-20, TASK 51-42-20-001-001-A01. MAJOR REPAIR.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 15,225 hrs · 10,716 cycles
TCAS DOUBLER CORRODED AT STINGER 27 BETWEEN BS 295 & 310. R & R TCAS DOUBLER IAW SRM 51-42-06-00-001-A0.
Part: SKIN — DENTED (BS 269-271) · airframe 15,234 hrs · 10,722 cycles
DENT BETWEEN BS 269 AND 271 STRINGESR 23 - 24 RT. FABRICATED DOUBLER IAW REO 690-53-11-631, SRM 51-24-16. MAJOR REPAIR.
2013
Part: LIGHT — MISSING (CABIN) · airframe 14,740 hrs · 10,388 cycles
MISSING APPROX 15 INCHES OF FLOOR EMERGENCY PATH STRIP ON LT SIDE OF FIRST CLASS CABIN. REPLACED MISSING EMERGENCY LIGHT, IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
Part: SKIN — CHAFED (BS 913) · airframe 13,992 hrs · 9,921 cycles
FUSELAGE SKIN CHAFED NEAR BS 913 AND STR 27. REPAIRED IAW REO 670-53-00-290. REPAIR CLASSIFED AS MAJOR.
Part: GLOWSTRIP — MISSING (GALLEY) · airframe 13,868 hrs · 9,840 cycles
GLOWSTRIP PARTIALLY MISSING ON GALLEY FLOOR. REPLACED GLOWSTRIP.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,987 hrs · 9,259 cycles
PAX DOOR AFT DRAG ANGLE CRACKED. R & R DRAG ANGLE SECTION IAW REO 670-52-11-072, REV E.
Part: LIGHT — MISSING (CABIN) · airframe 12,757 hrs · 9,136 cycles
EMERGENCY LIGHT STRIP MISSING FROM GALLEY FLOOR. REPLACED MISSING EMERGENCY LIGHT STRIP GALLEY FLOOR IAW AMM 33-51-01.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 12,469 hrs · 8,938 cycles
THE 8B AND 15D PASSENGER LIFE VEST BAGS TORN. REMOVED AND REPLACED SEAT 8B AND 15D PASSENGER LIFE VEST IAW AMM 25-61-03.
2012
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,614 hrs · 8,318 cycles
LEFT FS 280 CROSS BEAM CORRODED. REPAIRED IAW BOMBARDIER REO 670-53-11-612.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,614 hrs · 8,318 cycles
RIGHT FS 280 CROSSBEAM HAS CORROSION. REPAIRED IAW BOMBARDIER REO 670-53-11-612.
Part: SEAL — DEFECTIVE (EMERGENCY EXIT) · airframe 10,925 hrs · 7,761 cycles
THE 12A EMER EXIT PRESSURE SQUELL. REMOVED AND REPLACED OVERWING EMERGENCY EXIT SEAL AT 12A/B REF CRJ 900 AMM 52-21-07. PRESSURIZED A/C, NO LEAKS DETECTED REF CRJ 900 AMM 52-00-00.
2011
Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 9,434 hrs · 6,704 cycles
LT ENGINE FAN VIBE. LUBE FAN BLADES IAW AMM PERFORM GROUND FAN VIBE, OPS CHECK GOOD.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,370 hrs · 6,658 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED .5 INCH IN LENGTH. REPAIRED IAW SRM 52-11-04 TEMP REVISION 52-008.
Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 8,588 hrs · 6,146 cycles
VISUAL INSPECTED DUCTING AND AILC SELFTEST ALONG WITH ENG RUNS WITH BLEEDS CONFIGED. NO DEFECTS NOTED IAW AMM 71-00-00 AND 36-21-00 AIR RETURNED FOR LT BLEED DUCT WARNING MSG. MX INSPECTED DUCTING AND AILC. PERFORMED SELF TEST WITH ENG RUNS.
2010
Part: BUSHING — MISSING (ENGINE MOUNT) · airframe 7,043 hrs · 5,129 cycles
COMPANY DISPATCH RECALLED THE AIRCRAFT WHEN IT WAS SUSPECTED THAT A BUSHING MIGHT HAVE BEEN LEFT OUT OF THE UPPER CLEVIS MOUNT OF THE RIGHT ENGINE. THE RIGHT ENGINE HAD BEEN INSTALLED ON 10/24/2010. THE FLIGHT CREW ADVISED MIAMI ATC AND ASKED TO RETURN TO KATL. ATC VECTORED THE AIRCRAFT ON A HEADING TO KATL BUT BECAUSE OF WEATHER IN THE ATL AREA, THE FLIGHT CREW ELECTED TO DIVERT. THE DIVERSION WAS APPROVED AND AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KTYS. MAINTENANCE TOOK THE AIRCRAFT TO A HANGAR AND INSPECTED THE RIGHT ENGINE. THE BUSHING WAS CONFIRMED AS MISSING. MAINTENANCE REPLACED THE BUSHING AND RAN THE ENGINE. NO ABNORMAL VIBRATIONS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE FOLLOWING DAY, MAINTENANCE SUPERVISOR PERSONNEL DECIDED TO HAVE THE AIRCRAFT RETURNED TO THE HANGAR TO REPLACE THE CLEVIS AS A PRECAUTION. ON 10/28/10 THE AIRCRAFT ARRIVED AT KTYS HANGAR AND THE ENGINE WAS LOWER, THE CLEVIS REPLACED AND THE ENGINE REINSTALLED. POST MAINTENANCE ENGINE RUNS WERE ONCE AGAIN NORMAL FOR VIBRATION. ACCORDING TO GE REMOTE DIAGNOSTICS, AT NO TIME DID THE VIBRATION LEVEL OF THIS ENGINE EXCEED .4 MILS.
Part: COMPRESSOR — DAMAGED (RT ENGINE) · airframe 7,021 hrs · 5,116 cycles
ON TAKEOFF ROLL FROM KATL THE AIRCRAFT DEVELOPED A SEVERE NOSE WHEEL SHIMMY. THE FLIGHT CREW EXECUTED A REJECTED TAKEOFF AT APPROXIMATELY 85 KNOTS. DURING THE SLOWING OF THE AIRCRAFT WITH BRAKES AND THRUST REVERSERS, TOWER REPORTED SEEING SMOKE FROM THE RT ENGINE. CFR INSPECTED THE AIRCRAFT AND THERE WAS NO FIRE. THE AIRCRAFT WAS RELEASED TO THE GATE FOR PASSENGER DEPLANING. MAINTENANCE FOUND FOD DAMAGE TO THE FAN CASE OF THE RT ENGINE. FURTHER TROUBLESHOOTING BY BORESCOPE REVEALED DAMAGE TO THE FIRST AND SECOND STAGE COMPRESSOR BLISKS. THE AIRCRAFT WAS REMOVED FROM SERVICE AND THE ENGINE WILL BE REPLACED.
Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 6,995 hrs · 5,101 cycles
FUEL CH 1 FAIL STATUS MESSAGE, VERIFIED. REMOVED AND REPLACED FUEL QUANT COMPUTER IAW CRJ900 AMM 29-41-22. OPS CHECK GOOD, OK FOR CONT SERVICE.
Part: STRIP — MISSING (RADOME) · airframe 6,952 hrs · 5,066 cycles
RADOME DIVERTER STRIP MISSING FROM 10 O'CLOCK POSITION LOOKING AFT (UPPER RT REF). FLY ON AS IS FOR 200 FH WITHIN WHICH TIME RADOME WILL BE REPAIRED WITH NEW DIVERTER STRIP OR REPLACED.
Part: RESERVOIR — FAILED (HYDRAULIC SYS) · airframe 6,809 hrs · 4,959 cycles
HYD 2 HI TEMP CAUTION MSG IN-FLIGHT AIR RETURN TO ATL. REMOVED AND REPLACED RESERVOIR IAW AMM 29-10-00.
Part: ISOLATION VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 5,585 hrs · 4,148 cycles
DURING SINGLE PACK OPERATION AT FL250 BETWEEN ATL-PWM THE ISOL VALVE BEGAN OSCILLATING OPEN AND CLOSED. AS THIS WAS HAPPENING THE RT PACK BEGAN TO OPEN AND CLOSE. THE PACK WOULD THEN FREEZE. THE CABIN WAS BEGINNING TO CLIMB AND DESCEND AS WELL. NOTIFIED MOC AND DISPATCH. RETURNED TO ATL. THE DECISION WAS ALSO MADE BY FLIGHT CREW TO DESCEND TO 10000FT. CREW DIDNâT BELIEVE THE CABIN WAS GOING TO HOLD ANY LONGER. THE SITUATION WAS NOT IMPROVING. NOTIFIED DISPATCH, AND DISPATCH DECIDED ALONG WITH MOC FOR ACFT TO LAND TYS. LANDED UNEVENTFULLY, MAINT IN TYS WORKED ON ACFT, DEPARTED ON TO PWM. WHILE IN TYS THE ISO VALVE WAS OPERATIONALLY CHECKED IAW 36-13-15 AND DEEMED AIRWORTHY. AS OF 04/12/10 THERE HAVE BEEN NO REPEATS.
Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 5,554 hrs · 4,098 cycles
LT ENGINE BLEED VALVE OPENING AND CLOSING CRUISING LT PACK TO SHUT OFF. REMOVED & REPLACED ACSC1 PER CRJ900 AMM 21-61-04, OPS CHECKS GOOD. OK FOR SERVICE.