N299PQ
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.
91 reports on file, 2014-06-09 – 2024-02-07.
Part: ELECTRICAL BOX — CRACKED · airframe 22,705 hrs · 17,143 cycles
FOUND EXTERIOR POWER PLUG BOX SURROUND TO BE CRACKED. REMOVED EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: FRAME — DEFORMED (ZONE 100) · airframe 22,705 hrs · 17,143 cycles
FOUND 2EA ELONGATED HOLES ON FS 193 FOR EXTERIOR POWER PLUG BOX REPAIRED LOWER FRAME SECTOR, F.S.193 IAW ENDEAVOR AIR EA# CRJ953-16057 REV IR DATED 1/29/2024
Part: SKIN — CHAFED (ZONE 600 SLAT) · airframe 22,705 hrs · 17,143 cycles
R/H I/B SLAT HAS 2 AREAS OF CHAFFING ON AFT SIDE BY TELESCOPPING ANTI ICE DUCT. REPAIRED IAW ENDEAVOR AIR EA CRJ957-15996 REV IR DATE 1/16/2024 .
Part: VANE — CHAFED (ZONE 600 FLAP) · airframe 22,705 hrs · 17,143 cycles
"R/H I/B FLAP VANE IS CHAFED ON THE LEADING EDGE APPROX 8 INCHES FROM O/B EDGE. BLENDED DAMAGE IAW CRJ900 SRM 57-52-01-101-001-A01 TABLE 1 AND CRJ900 SRM 51-12-00-001-001-A01 PARAGRAPH 7, EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 57-52-01-101-001-A01, MAT. ORIGINAL 0.050"", MAT. REMOVED 0.020"", REMAINING THICKNESS 0.030"". REMOVED AND REPLACED PANEL 684HT."
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,705 hrs · 17,143 cycles
F.S.280 CROSSBEAM J ANGLE IS CORRODED BETWEEN LBL12 AND RBL12 REMOVED AND INSTALLED NEW J ANGLE AT FS280 WITH P/N CC670-34095-3S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: PANEL — CHAFED · airframe 22,705 hrs · 17,143 cycles
PANEL 684EB IS CHAFED REMOVED AND REPLACED NEW SERVICEABLE PANEL 684EB (PN CC670-1477-2) IAW CRJ900 SRM 51-40-11-001-001-A01
Part: RETAINER — DAMAGED (PAX DOOR) · airframe 22,705 hrs · 17,143 cycles
PERM REPAIR PAX DOOR RETAINER. INSTALLED NEW PAX DOOR SEAL RETAINER P/N 601R318722-1 IAW CRJ-900 SRM 52-11-07-201-001-A01.
Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 22,705 hrs · 17,143 cycles
R/H FWD OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED RH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16044 REV. IR DATED 1/27/2024.
Part: FRAME — CRACKED · airframe 22,705 hrs · 17,143 cycles
L/H FWD OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED LH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16042 REV. IR DATED 1/27/2024.
Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 22,705 hrs · 17,143 cycles
R/H AFT OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED RH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16043 REV. IR DATED 1/27/2024.
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 22,705 hrs · 17,143 cycles
AFT CARGO DOOR LOWER SILL HAS MULIPLE AREAS OF CORROSION. INSTALLED A NEW LOWER SILL (P/N: MM670-35655-003). IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 AND RESTORED SURFACE FINISH IAW CRJ 900 SRM (TR51-0068) 51-21-16-001-001-A01.
Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 22,705 hrs · 17,143 cycles
LH AFT OVERWING EMERGENCY EXIT DOOR TOP ALIGNMENT BRACKET IS CRACKED. REPAIRED LH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA#: CRJ952-16041 REV. IR DATED 1/27/2024.
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 22,705 hrs · 17,143 cycles
LH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF LH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01
Part: SEAL — TORN (APU EXHAUST) · airframe 22,705 hrs · 17,143 cycles
APU EXHAUST AFT B SEAL TORN AWAY FROM ATTACH FASTENERS LOWER SIDE BETWEEN 5:00 AND 7:00 POSITION. REMOVED AND REINSTALLED APU EXHAUST TAILCONE ASSEMBLY AS REQUIRED IAW CRJ 900 AMM TASK 53-85-00-000/400-801-A01. REMOVED AND REPLACED AFT APU EXHAUST BAND CLAMP, B SEAL AND RIVETS AS REQUIRED FOR REPLACEMENT IAW CRJ 900 AMM TASK 49-81-00-960-802 (CONFIG A01) . FABRICATED APU EXHAUST AFT B-SEAL BAND CLAMP OUT OF AISI321-AMS5510 0.020 (5-11472) IAW REO 670-49-81-006 DATED 2023-07-14 REV E.
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 22,705 hrs · 17,143 cycles
RH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF RH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 22,705 hrs · 17,143 cycles
LH AFT VERTICAL STAB DRAG ANGLE IS CRACKED INSTALLED SERVICEABLE DRAG ANGLE AFT, LH SIDE WITH PN AV670-21186-003 IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 22,705 hrs · 17,143 cycles
RH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. REPLACED RH AFT DRAG ANGLE USING P/N AV670-21186-004 IAW CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01.
Part: PANEL — CHAFED (ZONE 500 FLAP) · airframe 22,705 hrs · 17,143 cycles
"L/H WING FLAP PANELS 584HT AND 584ET HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRID CHAFFED AREA ON L/H WING FLAP PANELS 584HT AND 584ET ALLOWABLE DAMAGE 0.015"" IAW CRJ900 SRM 57-53-01-101-001-A02. PANEL 584HT FOUND TO BE IN LIMITS ORG. .050"", REMAINING .048"", ALLOWABLE .015"", REMOVED .002"". PANEL 584ET FOUND TO BE OUT OF LIMITS ORG. .050"", REMAINING .031"", ALLOWABLE .015"", REMOVED .019"". IAW CRJ 900 SRM 57-53-01-101-001-A02. LOCATED AND DRILLED NEW PANEL 584ET P/N CC670-14027-3, IAW CRJ-900 SRM 51-40-11-001-001-A01. PAINTED NEW PANEL 584ET IAW CRJ 900 SRM 51-25-01-001-001-A01."
Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 22,705 hrs · 17,143 cycles
PASSENGER DOOR SURROUND STRUCTURE, LOWER SILL MID CAP ANGLE IS CORRODED. REMOVED MID CAP ANGLE AS REQUIRED FOR REPLACEMENT IAW CRJ 900 SRM TASK 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL MID CAP ANGLE (PN# SH670-31825-9S) IAW CRJ900 SRM 51-41-02-001-001-A01
Part: STOP FITTING — CORRODED (AFT CARGO DOOR) · airframe 22,705 hrs · 17,143 cycles
AFT CARGO DOOR UPPER AND LOWER STOP FITTING HAVE LIGHT SURFACE CORROSION. REMOVED DAMAGE FROM AFT CARGO DOOR FWD UPPER AND LOWER STOP FITTINGS BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-16015 REV IR DATED 1/24/2024 AND EA CRJ953-16016 REV IR DATED 1/24/2024.
Part: PANEL — CHAFED (ZONE 500 FLAP) · airframe 22,705 hrs · 17,143 cycles
"L/H WING FLAP PANELS 584LB, 584JB, 584EB, AND 584GB HAVE CHAFFING AND PAINT DAMAGE. BLENDED AND GRIDDED CHAFED AREA ON 4EA L/H WING FLAP ACCESS PANELS 584LB, 584JB, 584EB, AND 584GB IAW CRJ900SRM 51-12-00-001-001-A01. PANELS 584LB, 584EB AND 584GB FOUND TO BE WITHIN LIMITS. PANEL 584JB FOUND TO BE OUT OF LIMITS. 584LB ORG. .090"", REMAINING .086"", ALLOWABLE .015"", REMOVED .004"". 584EB ORG. .090"", REMAINING .087"", ALLOWABLE .015"", REMOVED .003"". 584GB ORG. .090"", REMAINING .078"", ALLOWABLE .015"", REMOVED .012"". 584JB ORG. .090"", REMAINING .072"", ALLOWABLE .015"", REMOVED .018"" IAW CRJ900 SRM 57-52-01-101-001-A01. RESTORED FINISH IAW CRJ-900 SRM 51-25-06-001-001-A01 AND SRM 51-25-16-001-001-A01."
Earlier reports · 2014–2022 · 70 reports
2022
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,557 hrs · 15,229 cycles
EMERGENCY LIGHT ON LH SIDE 19TH PAX WINDOW INOPERATIVE. R & R EMERGENCY LIGHT LH SIDE IAW 33-51-15 . OPS TESTED GOOD.
Part: NONE — INOPERATIVE · airframe 20,216 hrs · 14,962 cycles
14962
2020
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,609 hrs · 10,952 cycles
EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT INOP. R/R'D NR 2 & NR 3 EMER LIGHT BATTERY PACKS IAW AMM 33-51-17. ALL CHECKS GOOD. ACFT OK FOR SVC.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,583 hrs · 10,931 cycles
FOUND EMERGENCY LIGHT EXTERIOR BY PAX DOOR INOP. REMOVED AND RELAMPED LIGHT BULB IAW AMM 33-51-15 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS310 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). " "FRAME FS310 BTW STGR 26L TO 26R WAS REPAIRED PER EA CRJ953-10298 REV IR "
Part: RETAINER — WORN (CARGO DOOR) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: BENT AND WEAR ON AFT CENTER SEAL RETAINER AT CENTER BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER AT CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM51-42-06-001-001-A01. "
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 15,136 hrs · 10,564 cycles
"PART RACKS: CORROSION ON RAILS (3EA) PN: BA690-30002-41, BA690-30002-43 AND BA690-30002-45 OF FWD CARGO COMPARTMENT.(SM)(CCD) " "CORROSION ON RAILS WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND REWORKED AREA ON RAIL PN: BA690-30002-45 IT IS WITHIN LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 AND RAILS PN:BA690-30002-41, BA690-30002-43 DUE TO DAMAGE EXCEEDS THE 20% OF THE THICKNESS ALLOWED, THEREFORE RAILS (2 EA) WERE REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01 "
Part: ACCESS PANEL — WORN (TE FLAP) · airframe 15,136 hrs · 10,564 cycles
"PART RACKS: WEAR ACCESS PANEL NBR 584EB AT LH INBD FLAP (SM). ""ACCESS PANEL 584EB WAS REPLACED FOR A ONE NEW P/N CC670-14177-1 PER CRJ900 SRM 57-52-01-001-001-A01 ITEM.10 "
Part: RETAINER — WORN (CARGO DOOR) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON INNER/OUTER SEAL RETAINER AT CENTER BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER ON CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM51-42-06-001-001-A01 "
Part: RETAINER — WORN (CARGO DOOR) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: BENT AND WEAR ON FWD/AFT LOWER CORNERS ON INNER/OUTER SEAL RETAINER AT FWD BAGGAGE BAY DOOR. (C1). ""SEAL RETAINER ON FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 15,136 hrs · 10,564 cycles
"PART RACKS: CORROSION ON RAILS (3EA) PN: BA690-30002-41, BA690-30002-43 AND BA690-30002-45 OF FWD CARGO COMPARTMENT.(SM)(CCD) ""CORROSION ON RAILS WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND REWORKED AREA ON RAIL PN: BA690-30002-45 IT IS WITHIN LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 AND RAILS PN:BA690-30002-41, BA690-30002-43 DUE TO DAMAGE EXCEEDS THE 20% OF THE THICKNESS ALLOWED, THEREFORE RAILS (2 EA) WERE REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01 "
Part: BEAM — CRACKED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CRACKED LONGITUDINAL BEAM LBL 12 AT UNION WITH XBEAM 280-. " "LONGITUDINAL BEAM LBL 12 AT UNION WITH XBEAM 280 WAS REPAIRED PER REO 690-53-11-1221 REV. -- AFTER IMPLEMENTATION OF THE REO 670-53-11-896 REV. -- "
Part: BEAM — CRACKED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CRACKED LONGITUDINAL BEAM RBL 12 AT UNION WITH XBEAM 280-. " "LONGITUDINAL BEAM RBL 12 AT UNION WITH XBEAM 280 WAS REPAIRED PER REO 690-53-11-1221 REV. -- AFTER IMPLEMENTATION OF THE REO 670-53-11-896 REV. -- "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR 25R BTW FS310 TO FS319. (E/E)(TCI: 53-20-304). " "STRINGER 25R BTW FS 280 TO FS 333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR 24R BTW FS319 TO FS333. (E/E)(TCI: TCI: 53-20-304). " "STRINGER 24R BTW FS280 TO FS333 WAS REPLACED FOR A NEW ONE PER CRJ900SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). ""INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). ""INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 15,136 hrs · 10,564 cycles
"PART RACKS: DELAMINATION ON FLOOR PANELS 282JRF, 282KRF, 282FRF, 282GRF, 281BLF, 281CLF, 281DLF, 281GLF, AND 281JLF(ALSO HAS A CORRODED INSERT) AFT CARGO COMPARTMENT C-2 " "SUMMARY: FLOOR PANELS 282KRF, 281JLF, 281DLF, 282GRF, 281CLF AND 281GLF AFT CARGO COMPARTMENT WERE REPAIRED PER CRJ-900 ATA 53 COMCMM-03 REV. T PAR. 10.2 ; NEW FLOOR PANEL 282FRF P/N:BA670-31683-7 WAS MODIFIED PER CRJ-900 TS#005400DWG. FAB-P16834 AND FLOOR PANELS 281BLF AND 282JRF WERE REPLACED FOR NEW ONE DUE TO DAMAGE DIMENSIONS ARE OUT OF LIMITS PER CRJ-900 ATA 53 COMCMM-030 REV. T PAR. 8.0 "
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON DOUBLER OF FWD TCAS ANTENNA BTW FS 295 TO FS310, STGR 26L TO 26R. (E/E)(TCI:53-20-304). ""DOUBLER OF FWD TCAS ANTENNA BTW FS 295 TO FS310 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). " "INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"AWR; [ TASK R53520 STEP 7 ]; CORROSION ON SUPPORT FITTING BETWEEN FS 285 AND 17RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX). ""SUPPORT FITTING WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-21-001-001-A01. "
Part: SCUFF PLATE — DENTED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"PART RACKS: SEVERAL DENTS ON SCUFF PLATE OF SOURROUND STRUCTURE AT THE FWD/CENTER BAGGAGE BAY DOORS (CCD). " "SCUFF PLATES (151MLW AND 151ZLW) OF SOURROUND STRUCTURE AT THE FWD/CENTER BAGGAGE BAY DOORS WERE REPLACED FOR A NEW ONES PER CRJ900 AMM 25-52-01 "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. (TCI 53-20-313)(E/E). " "INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS319 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). ""FRAME FS319 BTW STGR 26L TO 26R WAS REPAIRED PER EA N°: CRJ953-10299 REV IR. "
Part: STRAP — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
PART RACKS: CORROSION ON FWD STRAPS AT ACCESS PANEL 193AB. (FUS). "STRAPS (2EA, P/N:CC670-39052-3S AND CC670-39052-4S) ON ACCESS PANEL 193AB WERE REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-10-001-001-A01. "
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS295 BTW STGR 26L TO 26R. (E/E)(TCI:53-20-304). " "FRAME FS295 BTW STGR 26L TO 26R WAS REPAIRED PER EA N°: CRJ953-10297 REV IR. "
Part: FRAME — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON FRAME FS349 BTW STGR 26L TO 26R. (E/E)(TCI: 53-20-304). ""FRAME STA 349 BTW S23L TO S24R WAS REPLACED FOR A NEW ONE PER CRJ-900SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR 26R BTW FS295 TO FS310. (E/E)(TCI: TCI: 53-20-304). " "STRINGER 26R BTW FS280 TO FS330 WAS REPLACED FOR A NEW ONE PER CRJ900SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. "
Part: SEAL — WORN (VERTICAL STAB) · airframe 15,136 hrs · 10,564 cycles
"POST-PATR RACKS : WORN AND LOOSE TEFLON SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR ( EHV ) " "SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-22-00-001-001-A01 "
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON LOWER SILL ANGLE AT PASSENGER DOOR EXTERNAL SURROUND. (TCI 53-20-220). ""LOWER SILL ANGLE AT PASSENGER DOOR EXTERNAL SURROUND WAS REPLACED PERCRJ-900 SRM 51-42-06-001-001-A01 LEVEL CORROSION 2 "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS280 TO FS295. (E/E)(TCI:53-20-304). ""STRINGER 27 BTW FS280 TO FS295 WAS REPLACED FOR A NEW ONE PER CRJ-900SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 "
Part: COAMING — WORN (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: WEAR SEVERAL PLACES AROUND AFT BAGGAGE-BAY DOOR CUT OUT CARGO-2 TCI: 53-30-204 ""(LOWER COAMING) AFT BAGGAGE-BAY DOOR CUT OUT CARGO-2 WAS REPLACED PERCRJ-900 SRM 51-41-02-001-001-A01 "
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION STGR SPLICE 26R AT FS333. (E/E)(TCI: 53-20-304). ""STRINGER SPLICE 26R AT FS 333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. (LEVEL CORROSION 2). "
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR SPLICE 25R AT FS333. (E/E)(TCI:53-20-304). " "STRINGER SPLICE 25R AT FS333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01. (LEVEL CORROSION 2). "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STGR 26R BTW FS333 TO FS364. (E/E)(TCI: 53-20-304). ""STRINGER 26R BTW FS333 TO FS364 WAS REPLACED FOR A NEW ONE PER CRJ900SRM 51-42-06-001-001-A01. (LEVEL CORROSION 2) "
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON STGR SPLICE 24 RH AND FS:333 AT FWDAVIONICS COMPARTMENT (E/E) (TCI:53-20-304) ""STRINGER SPLICE 24RH AND FS 333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. (LEVEL CORROSION 2). "
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON LOWER MD CAP ANGLE AT PASSENGER DOOR EXTERNAL SURROUND. (TCI 53-20-220) " "LOWER MID CAP ANGLE AT PASSENGER DOOR EXTERNAL SURROUND WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-001-A01 LEVEL CORROSION 2. "
Part: ACCESS PANEL — GOUGED (LT WING) · airframe 15,136 hrs · 10,564 cycles
"DAMAGE T. DURING LH WING FUEL ACCESS PANEL INSTALL, GOUGE WAS FOUND ON ACCESS PANEL 551FB. " "SUMMARY: FUEL ACCESS PANEL 551FB AT LH WING WAS REPLACED PER CRJ900 AMM 28-11-01. "
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON RH FLOOR SILL BTW FS 280-319 AT PASSENGER CABIN. (TCI 53-20-315). " "FLOOR SILL BTW FS280 TO FS319 WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01. CORROSION LEVEL 2 "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON STRINGER 21R BTW FS 333-349 AT MAIN AVIONICS COMPARTMENT. (TCI 53-20-305). ""STRIGER 21R BTW FS333-349 WAS REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. "
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON STGR 18RH BTW FS:295 TO FS:310 AT FWD AVIONICS COMPARTMENT (E/E) (TCI:53-20-304) " "CORROSION LEVEL 2: STRINGER 18RH BTW FS280 TO FS310 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. "
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION. CORROSION ON INTERCOSTAL BTW FS 349-364 STRG 20R AT MAIN AVIONICS COMPARTMENT. (TCI 53-20-305). " "INTERCOSTAL WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01. NIVEL 2 "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON STGR 22RH BTW FS:280 TO FS:333 AT FWD AVIONICS COMPARTMENT (E/E) (TCI:53-20-304) " "STRINGER 22RH BTW FS:280 TO FS:333 AT FWD AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 21R, 22R, FS 333. (TCI: 53-20-304). " "STRINGERS SPLICE 21R, 22R, FS 333. WERE REPLACE FOR A NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. CORROSION LEVEL 2. "
Part: COAMING — WORN (LT ENGINE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: WEAR ON LATCH DOOR COAMING EXTERNAL FACE AT LH ENGINE. (SM)(MOT 1) " "COAMING LATCH DOOR AND DOUBLER WERE REPLACED PER CRJ900 SRM 54-21-00-101-001-A01 AND SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01 "
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON AFT WATER WASTE SERVICE PANEL GREENLIGHT SUPPORT FITTING ( FUS) ( TCI: :100-19) " "GREEN LIGHT SUPPORT FITTING ON AFT WATER WASTE SERVICE PANEL WAS REPLACED FOR A NEW ONE PER CRJ 900 SRM 51-41-02-001-001-A01. (LEVEL CORROSION 2). "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON SIDE SEAT RAILS STRG 15R & 15L BTWFS 744 TO FS 761 AT PAX CABIN (CPAX)(TCI 53-20-233). ""SIDE SEAT RAILS STRG 15R & 15L BTW FS 744 TO FS 761 AT PAX CABIN WEREREPLACED PER CRJ-900 AMM 53-00-49-400-801-A12. LEVEL CORROSION 2 "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION : CORROSION ON SIDE SEAT RAILS STRG 15R BTW FS 785TO FS 913 AT PAX CABIN (CPAX)(TCI 53-20-233). " "SIDE SEAT RAILS STRG 15R BTW FS 785 TO FS 913 AT PAX CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12 LEVEL CORROSION 2. "
Part: STRINGER — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON STRINGER 21R BTW FS 310-333.(TCI: 53-20-304). ""STRINGER 21R FROM STA.280 TO STA.333 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. CORROSION LEVEL 2 "
Part: ANGLE — CRACKED (PAX DOOR) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CRACK ON ANGLE BTW AFT SIDE PANEL AND INNER SKIN NEAR OF ACCESS PANEL 832DR AT PASSENGER DOOR. (L1). " "ANGLE BTW AFT SIDE PANEL AND INNER SKIN NEAR OF ACCESS PANEL 832DR AT PASSENGER DOOR WAS REPLACE PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR 6.C. AND CRJ-900 S.R.M. 51-42-13-001-001-A01 PAR 6.C AND CRJ-900 S.R.M. 51-42-22-001-001-A01 PAR. 6.C "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"AWR; [ TASK R53520 STEP 7 ]; CORROSION SEAT TRACK 27LBL FS 364 AT PAX CABIN FWD WET AREA. (W1) (CPAX). ""SEAT TRACK 27LBL FS 364 TO 485 AT PAX WASREPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.LEVEL CORROSION 2. "
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,136 hrs · 10,564 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 373 TO FS= 485, 9LBL ] [ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-243). ""FLOOR SEAT RAILS IN SECTIONS [ FS= 373 TO FS= 485, 9LBL ] [ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12 LEVEL CORROSION 2 "
2018
Part: SIGN — INOPERATIVE (CABIN) · airframe 11,691 hrs · 7,984 cycles
CABIN CIELING EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PS36 IAW AMM 33-51-17. OPS CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME.
Part: OXYGEN MASK — BROKEN (FLIGHT DECK) · airframe 11,548 hrs · 7,876 cycles
CAPTAIN`S OXYGEN MASK RED SWITCH TO TEST BROKEN. REMOVE & REPLACE THE OXYGEN MASK IAW AMM 35-11-12-000-801. MASK TESTED GOOD. ACFT OK FOR SERVICE.
Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 11,320 hrs · 7,710 cycles
CA SIDE O2 MASK RED TAB BROKEN OFF. R&R CREW O2 MASK IAW AMM 35-11-12. OPS CHECK NORMAL AT THIS TIME.
Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 11,103 hrs · 7,552 cycles
FLASHLIGHT UNDER FLIGHT ATTENDANT JUMPSEAT NOT FLASHING. REMOVED AND REPLACED THE FLASHLIGHT POWER UNIT IAW CMM 25-60-11. OPS CHECKED GOOD.
Part: RESERVOIR — INOPERATIVE (HYDRAULIC SYS) · airframe 10,029 hrs · 6,808 cycles
DURING L/G RETRACTION "HYD PUMP 3A CAUTION" FOLLOWED BY GEAR DISAGREE WARNING DUE TO N/W VERY SLOWLY RETRACTING. NLG FULLY RETRACTED APPROXIMATELY 20 SECONDS LATER & AYL MESSAGES WENT OUT AND SYSTEM 3 SHOWED NORMAL AGAIN. R&R NR 3 HYDRAULIC RESERVOIR IAW AMM 29-12-30 & PERFORMED NR 3 ACCUMULATOR PRESSURE-DECAY RATE IAW AMM 29-12-11. RESERVOIR PN(ON) 960450-1 (OFF)960450-1. SN(OFF) 0286 (ON) 0951. SEE NON-ROUTINE WORK CARD 633814 FOR DETAILS. NR 3 ACCUMULATOR PN OFF 900122-1 ON 900122-1 SN OFF.
2017
Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 8,284 hrs · 5,604 cycles
CAPTAIN`S OXYGEN MASK DOES NOT TEST PROPERLY. SWAPPED OBSERVER`S OXYGEN MASK WITH CAPTAIN`S AND PREFORMED OPS CHECK IAW AMM 35-31-00. REMOVED AND REPLACED THE OXYGEN MASK.
Part: CONTAINER — TORN (LIFE VEST) · airframe 7,976 hrs · 5,381 cycles
INFANT LIFE VEST BAG TORN. REPLACED THE LIFE VEST IAW AMM 25-61-03.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,752 hrs · 5,220 cycles
FS 280 BEAM CORRODED AT RBL 11 OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM FS 280 RIGHT SIDE IAW SRM 51-42-06, 51-42-11 AND 51-42-21.
Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 7,752 hrs · 5,220 cycles
E&E BAY RT CENTER DIAPHRAGM CORRODED ON FWD CORNER. NO ALLOWABLE LIMITS PER SRM 53-21-23. REMOVED AND REPLACED DIAPHRAGM IAW SRM 51-42-06, 51-42-21.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,752 hrs · 5,220 cycles
FS 280 BEAM CORRODED AT LBL 11 OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM AT FS 280 LEFT SIDE IAW SRM 51-42-21, 51-42-11 51-42-06.
Part: HOUSING — CRACKED (E&E DOOR) · airframe 7,752 hrs · 5,220 cycles
AVIONICS BAY COMPARTMENT DOOR HANDLE HOUSING IS CRACKED AROUND BASE OF HANDLE SHAFT. REMOVED AND REPLACED AVIONICS BAY HANDLE AND HOUSEING IAW SRM 51-42-21. PERFORMED OPS CHECK, OPS CHECK GOOD IAW AMM 52-42-00-710-801.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 7,752 hrs · 5,220 cycles
RIGHT FLOOR SILL CORRODED AT FS280.00. REPAIR RT FLOOR SILL AT FS 280.00 IAW REO 670-53-00-390 & REO 670-53-21-139 REV A.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,752 hrs · 5,220 cycles
MAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REMOVED THE DAMAGAE AND REPAIRED THE DRAG ANGLE IAW REO 670-52-11-072 REV.G.
2016
Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 6,709 hrs · 4,500 cycles
FORWARD FLIGHT AFT FLASHLIGHT IS NOT CHARGED. REPLACED THE FLASHLIGHT ASSY IAW AMM 25-61-02. OP CHECKED GOOD. OK FOR SERVICE.
2015
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 5,021 hrs · 3,374 cycles
CAPTAINS EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR EMER FLASHLIGHT IN FLIGHT STATION PILOTS SIDE IAW AMM 25-60-00.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 3,062 hrs · 2,004 cycles
F/A JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED FWD F/A EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-00. OPS CK GOOD.
Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 2,996 hrs · 1,961 cycles
UPON TAKEOFF RECEIVED A GEAR DISAGREE WARNING. HYD FLUID SHOWING 50% BUT BOTH 3AB PUMPS WERE YELLOW WITH NO HYD 3 PRESS GEAR DISAGREE, DISAGREE FIXED ITSELF, GEAR CAME UP & 3A PUMP WAS RUNNING. FLUID ON HYD 3 NOW 35% GEAR ALSO CAME DOWN NORMALLY. FOUND AIR IN HYD SYS NR 3. BLEEDING OF HYD SYS NR 3 TO REMOVE AIR IAW AMM 29-10-00. PERFORMED JACKING OF THE ACFT IAW AMM 07-11-01 TO SWING GEARS. PERFORMED FUNCTIONAL TEST OF LG EXTENSION & RETRACTION SYS IAW AMM 32-30-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE. HYD SYS NR 3 WAS LOW, SERVICED SYS 3 IAW AMM 12-12-29.
2014
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 1,231 hrs · 816 cycles
FORWARD FLIGHT ATTENDANT FLASHLIGHT SEAL IS BROKEN, FLASHLIGHT HAS NO CHARGE. R & R FWD FLIGHT ATTENDANT BULKHEAD EMER FLASHLIGHT ASSEMBLY & HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.