N181GJ
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.
68 reports on file, 2015-07-27 – 2025-10-22.
Part: LOCK — INOPERATIVE (ZONE 800) · airframe 29,529 hrs · 24,033 cycles
CA WENT TO USE BATHROOM AND COMING BACK THE FLIGHT DECK DOOR WOULD NOT OPEN. CA TRIED TO SHIMMY THE DOOR AND IT DID NOT OPEN SO WE HAD TO TAKE THE HINGE PIN OUT. R/R COCKPIT DOOR LOCK ASSY IAW CMM 25-17-03 OPC GOOD
Part: DIAPHRAGM — DAMAGED (ZONE 200) · airframe 28,179 hrs · 22,921 cycles
UPON LOCATING OF NEW RBL 36 BEAM, WE HAVE DISCOVERED DIAPHRAGM @ FS 792 ON RIGHT HAND SIDE TO HAVE MULTIPLE ELONGATED HOLES COMMON TO SILL DECK AND DIAPHRAGM. THESE HOLES ARE ONLY ELONGATED IN THE DIAPHRAGM, NOT ELONGATED IN THE SILL DECK SKIN. COMPLIED WITH MHIRJ SNIEO SH670-36126 IDENTIFIER S01 AND MHIRJ SNIEO SH690-36153 IDENTIFIER S03. WORK ACCOMPLISHED UNDER MHIRJ BARCODE HN00227022.
Earlier reports · 2015–2024 · 66 reports
2024
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 26,242 hrs · 21,276 cycles
PAX DOOR DD6 MID INTERCOSTAL CORRODED. LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 26,242 hrs · 21,276 cycles
MAIN AVIONICS DOOR HANDLE HOUSING HAS CRACK INDICATIONS FOUND AROUND CIRCUMFERENCE OF HANDLE BASE. FAILED NDT. REMOVED DOOR HANDLE HOUSING FROM MAIN AVIONICS COMPARTMENT DOOR IAW CRJ900 AMM 52-42-03-000-801-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE DOOR HANDLE HOUSING ON MAIN AVIONICS COMPARTMENT DOOR IAW CRJ900 AMM 52-42-03-400-801-A01 AND SRM 51-42-21-001-001-A01.
Part: STRIKER — CORRODED (SERVICE DOORSEAL) · airframe 26,242 hrs · 21,276 cycles
SERVICE DOOR SEAL STRIKER AFT SIDE HAS LIGHT CORROSION AROUND SCREW HOLES. REMOVED CORROSION IAW CRJ-900 SRM 51-21-06-001-001-A01 ORIGINAL MATERIAL THICKNESS 0.120 REMOVED .066 , REMAINING MATERIAL THICKNESS 0.054, SEAL STRIKER IS OUT OF LIMITS DUE TO MORE THEN 10% MATERIAL LOSE AND NO DAMAGE ALLOWED AROUND 2D OF A FASTENER HOLE, REQUIRED REPLACEMENT. LOCATED AND DRILLED NEW SERVICE DOOR SEAL STRIKER (P/N:SH670-31412-7) IAW CRJ900 SRM 51-40-11-001-001-A01, INSTALLED NEW SERVICE DOOR SEAL STRIKER (P/N:SH670-31412-7) IAW CRJ900 SRM 51-42-06-001-001-A01.
Part: DOOR FRAME — CRACKED (RT EMER EXIT) · airframe 26,242 hrs · 21,276 cycles
R/H FWD. EMERGENCY EXIT DOOR S/N: SB0836 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16164, REV IR, DATED 3/28/2024.
Part: ANGLE — CORRODED (ZONE 200) · airframe 26,242 hrs · 21,276 cycles
SERVICE DOOR ANGLE MOUNTING HAS HEAVY CORROSION. REMOVED ANGLE MOUNTING (P/N:SH670-31996-3) IAW CRJ900 SRM 51-21-06-001-001-A01. INSTALLED ANGLE LOWER SILL (P/N:SH670-31986-1) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW ANGLE MOUNTING IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED ANGLE MOUNTING (P/N:SH670-31996-3) IAW CRJ900 SRM 51-21-06-001-001-A01. FILLET SEALED AND RESTORE FINISH REPAIR AREA IAW CRJ 900 SRM 51-26-00-001-001-A01 AND SRM 51-23-00-001-001-A01
Part: DOOR FRAME — CRACKED (LT EMER EXIT) · airframe 26,242 hrs · 21,276 cycles
L/H AFT EMERGENCY EXIT DOOR S/N: SB0834 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16163, REV IR, DATED 3/25/2024.
Part: DOOR FRAME — CRACKED (RT EMER EXIT) · airframe 26,242 hrs · 21,276 cycles
R/H AFT EMERGENCY EXIT DOOR S/N: SB0830 - 1 (EA.) TOP FORMER CRACKED BY THE SWITCH TARGET. REPAIRED IAW ENDEAVOR AIR EA# CRJ952-16162, REV IR, DATED 3/25/24.
Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 26,242 hrs · 21,276 cycles
LH FS 280 BULKHEAD LOWER WEB AT LBL11 WL 72 IS CORRODED. L/H FS 280 LOWER WEB IS CORRODED ON MORE THAN ONE ELEMENT, DEPTH OF CORROSION IS .017 AND IS OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01.COMPLIED WITH STEPS 5.B.(1 THRU 3) REMOVE SPLICE PLATE, CUT LOWER WEB, AND DEBURR FOR L/H FS 280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01 FABRICATED, LOCATED AND DRILLED NEW L/H FS280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-003-A01, 51-24-36-001-001-A01 AND 51-40-11-001-001-A01.PO # FOR METAL USED IS 5-5501COMPLIED WITH ALL REMAINING STEPS FOR L/H FS 280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01. REMOVED AND REPLACED INCORRECTLY SHOT RIVETS IN FS 280 L/H LOWER WEB REPAIR IAW CRJ 900 SRM 51-42-13-001-001-A01 LOCATED, DRILLED AND INSTALLED 1 EACH MISSING FASTENER IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01 COMPLIED ALL REMAINING STEP IAW CRJ-900 SRM 53-11-10-201-004-A01.: COMPLIED IAW CRJ 900 SRM 53-11-10-201-004-A01, STEP 5.B (7), (PAINT ON FWD AND AFT SIDES OF LOWER WEB)COMPLIED IAW CRJ 900 SRM 53-11-10-201-004-A01.STEP 5.B (9) (IDENTIFIED REPAIR PARTS ON BUTTSTRAP PN: 53-11-10-201-004-A01-3 AND LOWER WEB PN: 53-11-10-201-004-A01-1). COMPLIED IAW CRJ 900 SRM 53-11-10-201-004-A01. STEP 5.B (10), CIC ON FWD SIDE OF LOWER WEB)
Part: SKIN — CHAFED (ZONE 800) · airframe 26,242 hrs · 21,276 cycles
"RIGHT MLG DOOR INNER SKIN AFT SIDE IS CHAFED APPROX. .5""W X 4""L X .010""D UPON FURTHER INVESTIGATION, CHAFE DAMAGE IS LOCATED ON R/H MLG DOOR INNER SKIN FILLER ON FWD SIDE. CHAFE IS APPROX. 0.010"" D AND RUNS ACROSS ENTIRE LENGTH OF PART. REMOVED DAMAGED FILLER AND FABRICATED, LOCATED, DRILLED NEW SERVICEABLE FILLER P/N CC670-10567-1 OUT OF 2024-T3 0.063"" (P.O.# 5-6156) IAW CRJ-900 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01 AND BOMBARDIER DWG CC670-10567 AND INSTALLED IAW CRJ-900 SRM 51-42-06-001-001-A01."
Part: COAMING — DEFORMED (ZONE 400) · airframe 26,242 hrs · 21,276 cycles
UPPER L/H TRANSCOWL LATCH DOOR COAMING, AND DOUBLER FOUND TO BE CHAFED AND SPIGOT HOLES ENLARGED. REMOVED UPPER L/H TRANSCOWL FWD LATCH TO F.O.M IAW CRJ900 SRM 51-41-02-001-001-A01 REMOVED FWD UPPER LATCH STIFFENER TO F.O.M IAW CRJ900 SRM 51-42-13-001-001-A01 REMOVED COAMING AND DOUBLER FOR REPLACEMENT IAW CRJ900 SRM 51-42-13-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01 LOCATED AND DRILLED SERVICEABLE COAMING (P/N: CN624-2060-209) & DOUBLER (P/N: CN624-2068-209) IAW CRJ 900 SRM 51-40-11-001-001-A01. RECEIVED, LOCATED AND DRILLED 1EA AFT LATCH BEARING PAD (P/N CN624-2130-201) IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED UPPER L/H TRANSCOWL FWD LATCH IAW CRJ 900 AMM 78-33-03-400-801(A01). INSTALLED SAME SERVICEABLE FWD UPPER LATCH STIFFENER IAW BOMBARDIER REO# 670-54-21-1207 REV. A DATED 2015-08-27. INSTALLED SERVICEABLE COAMING (P/N: CN624-2060-209) AND DOUBLER (P/N: CN624-2068-209) IAW CRJ 900 SRM 51-42-06/13-001-001-A01. RIGGED UPPER LH TRANSCOWL FWD LATCH IAW CRJ 900 AMM 78-30-00-820-801-A01. PERFORMED OPS CHECK OF THE UPPER LH TRANSCOWL FWD LATCH IAW CRJ 900 AMM 78-33-03-400-801-A01 5. D. OPS CHECK GOOD AT THIS TIME.
Part: DOOR FRAME — CORRODED (MAIN DOOR) · airframe 26,242 hrs · 21,276 cycles
PAX DOOR FWD FORMER IS CORRODED ON INNER SIDE. REMOVED DAMAGED FORMER, LOCATED, DRILLED AND INSTALLED SERVICEABLE PAX DOOR FWD FORMER, P/N 601R318031-5S IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 ,51-42-21-001-001-A01 AND 51-40-11-001-001-A01
Part: DRAIN PAN — DEFORMED (ZONE 100) · airframe 26,242 hrs · 21,276 cycles
FS 280 RH DRAIN PAN HAS SEVERAL ELONGATED HOLES AND POPPED RIVETS. REPAIRED IAW ENDEAVOR AIR EA CRJ953-16255 REV A DATED 3/25/2024.
Part: ANGLE — CORRODED (ZONE 800) · airframe 26,242 hrs · 21,276 cycles
SEVERAL AREAS OF CORROSION ON LH LNBOARD MLG DOOR REMOVED LIGHT CORROSION FROM EXPOSED SURFACE OF ANGLE P/N CC670-10563-3 PER CRJ 900 SRM 51-21-06-001-001-A01. RECEIVED AND COMPLIED WITH ALL STEPS OF ENDEAVOR AIR EA CRJ952-16169 REV IR DATED 3/18/2024.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,242 hrs · 21,276 cycles
"L/H FS 280 CROSSBEAM IS CORRODED BETWEEN BL0 AND LBL 5 UPON CLEANING UPPER FLANGE AND VERTICAL WEB OF FS280.00 FLOOR BEAM FROM BL 0 TO LBL 11 PER CRJ 900 SRM 51-26-00-001-001-A01, FOUND ADDITIONAL CORROSION ON UPPER FLANGE BETWEEN LBL 8 AND LBL 11. BEGAN REMOVING CORROSION FROM UPPER FLANGE PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND HEAVY PITTING. WITHOUT REMOVING ALL OF THE CORROSION THE BLEND IS .034"" DEEP, NOMINAL THICKNESS OF THE BEAM FLANGE AT THIS LOCATION IS .060", LEAVING AN MRT OF .026". INSTALLED L/H FS 280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, & 51-42-21-001-001-A01. LOCATED & DRILLED NEW CROSSBEAM IAW SRM 51-40-11-001-001-A01. REPLACED THE FLOORBEAM.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,242 hrs · 21,276 cycles
FS280 CROSSBEAM FWD J-ANGLE IS CORRODED AROUND FASTENER RECEPTACLES. LOCATED AND DRILLED NEW J-ANGLE P/N CC670-34095-1SB LOCATED AT FS 280 BETWEEN RBL 12 TO LBL 12 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW J-ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,242 hrs · 21,276 cycles
R/H FS 280 CROSSBEAM IS CORRODED BETWEEN BL0 AND RBL 5 REPLACED RH FS280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01,51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
Part: BULKHEAD WEB — CORRODED (ZONE100) · airframe 26,242 hrs · 21,276 cycles
RH FS280.00 BULKHEAD LOWER WEB IS CORRODED ON AFT FACE AT RBL 42, WL 72. REPAIRED RH FS280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01
Part: SKIN — CORRODED (RT MLG DOOR) · airframe 26,242 hrs · 21,276 cycles
SEVERAL AREAS OF CORROSION ON THE RIGHT MLG DOOR SKIN ON FORWARD INBOARD EDGE. REMOVED CORROSION FROM R/H MLG I/B DOOR FWD EDGE MEMBER (CC670-10524-4 0.063"") IAW CRJ-900 SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED IAW CRJ-900 SRM 52-82-02-101-001-A01. ENGINEERING REQUIRED. PERFORMED U.T. THICKNESS ON R/H I/B MLG DOOR REWORK AREAS IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 02/08/2022. FOUND LOWEST REMAINING THICKNESS TO BE .054"" OR GREATER. MEASUREMENTS RECORDED ON PHOTO IN ATTACHMENTS. RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA CRJ952-16166 REV IR DATED 3/18/2024. "
Part: FITTING — WORN (RUDDER) · airframe 26,242 hrs · 21,276 cycles
"MID LOWER RUDDER FITTING BOTTOM HALF BEARING BORE IS WORN. DEPTH SHOULD BE .286"" BORE IS AT .3185"" FITTING REQUIRES REPLACEMENT. LOCATED AND DRILLED FASTENER HOLES IN NEW SERVICEABLE FITTING PN AV670-21081-013 IAW CRJ 900 SRM 51-40-11-001-001-A01. REFERENCE HN00145134 FOR INSTALLATION OF FITTING. MACHINED EXCESS MATERIAL FROM NEW MID LOWER RUDDER FITTING AS REQUIRED IAW DWG AV670-21081-101 REV -B STEP 14. PRIMED AND PAINTED MID /LOWER RUDDER FITTING IAW CRJ SRM TASK 51-25-16-001-001-A01. "
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,242 hrs · 21,276 cycles
RH FLOOR SILL IS CORRODED AT FS 280. REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS 280 TO FS 319 IAW CRJ-900 SRM 51-21-06-001-001-A01.
Part: BUSHING — DAMAGED (ZONE 500 AILERON) · airframe 26,242 hrs · 21,276 cycles
UPON REMOVAL OF L/H AILERON SIDE PCU BUSHINGS, BUSHING LUGS FOUND TO BE PREVIOUSLY OVERSIZED REPAIRED LH AILERON PCU BUSHING LUGS IAW REO 670-57-6-237 REV - - DATED 2017-07-25
Part: FORMER — CRACKED (ZONE 800) · airframe 26,242 hrs · 21,276 cycles
L/H FWD. EMERGENCY EXIT DOOR S/N: SB0835 - 2 (EA.) TOP FORMERS CRACKED BY THE SWITCH TARGET. REPAIRED IAW MHIRJ REO 690-52-162.
Part: ANGLE — CRACKED (DOOR STEP) · airframe 26,242 hrs · 21,276 cycles
AFT STEP PANEL. CRACKS AT RIVET. MARKED WITH ORANGE TAPE. NEXT TO PULLEY BRACKET. REMOVED, LOCATED, DRILLED AND INSTALLED SERVICEABLE PAX DOOR AFT DRAG ANGLE, P/N 601R31772-5, IAW CRJ 900 SRM 51-40-11-001-001-A041 AND 51-42-06-001-001-A01UPON FURTHER INVESTIGATION FOUND PAX DOOR DRAG ANGLE WAS PREVIOUSLY REPAIR AND AFTER REMOVAL OF REPAIR FOUND ELONGATED HOLES IN PAX DOOR STAIR WEB AND INNER SKIN. THE UPPER EXISTING CUTLINE IS LOCATED IN THE WRONG LOCATION. ENGINEERING IS REQUIRED FOR ELONGATED HOLES AND INCORRECT CUTLINE IAW CRJ 900 SRM 52-11-04-201-002-A01. PAX DOOR AFT DRAG ANGLE P/N 601R31772-5 IS CRACKED AND REQUIRES REPAIR IAW CRJ-900 SRM 52-11-04-201-002-A01. REFERENCE LINE ITEM 1B FOR REPLACEMENT OF AFT DRAG ANGLE, HN00146304 FOR REPLACEMENT OF THE INNER SKIN PANEL, AND HN00146773 FOR REPLACEMENT OF THE AFT STAIR WEB. REFERENCE HN00146268 FOR INSTALLATION OF POWER ASSIST PULLEY BRACKET.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 26,242 hrs · 21,276 cycles
RH AFT VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. INSTALLED RH AFT DRAG ANGLE (PN:AV670-21186-004) IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.
Part: DRAG ANGLE — CRACKED · airframe 26,242 hrs · 21,276 cycles
RH FWD VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. REPAIRED RH FWD VERTICAL DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 26,242 hrs · 21,276 cycles
LH FWD VERTICAL DRAG HAS A POSSIBLE CRACK REPAIRED LH FWD DRAG ANGLE IAW CRJ-900 SRM 55-31-00-201-001-A01.
Part: WEB — CRACKED (ZONE 100) · airframe 26,242 hrs · 21,276 cycles
FWD EQUIPMENT COMPARTMENT L/H FLOOR WEB IS CRACKED AT F.S.193. INSTALLED NEW FRAME CLEAT @ FS193 PER REPAIR IAW CRJ900 SRM 53-11-43-201-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01. INSTALLED REPAIR PARTS IAW CRJ900 SRM 53-11-43-201-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01. APPLIED PAINT AND FINISH ON REPAIR AREA IAW CRJ900 SRM 51-42-06-001-001.
2020
Part: ANGLE — CORRODED (BS 333) · airframe 19,630 hrs · 15,566 cycles
PASSENGER DOOR LOWER SILL ANGLE IS CORRODED AT FS 333.00. REMOVED PAX DOOR LOWER SILL ANGLE THAT WAS CORRODED AT FS 333.00, IAW CRJ 900 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE AT FS 333.00 P/N: SH670-31875-75 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: DOUBLER — CORRODED (TACAS ANTENNA) · airframe 19,630 hrs · 15,566 cycles
TCAS DOUBLER IS CORRODED. REMOVED AND REPLACED TCAS DOUBLER, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 661-672) · airframe 19,630 hrs · 15,566 cycles
PAX FLOOR SEAT TRACK BETWEEN FS 661+32 AND FS 672.00 LBL 9 IS CORRODED. REMOVED, FABBED, AND INSTALLED SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343 AND AMM 53-00-49-000/400-801-A13.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,630 hrs · 15,566 cycles
FLOOR SEAT TRACK CORRODED AT RBL 9 BETWEEN FS 847+51 TO FS 977. FABBED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-343 AND CRJ 900 AMM 53-00-49-000/400-801-A13.
Part: SEAT TRACK — CORRODED (BS 409-485) · airframe 19,630 hrs · 15,566 cycles
CABIN FLOOR SEAT RAIL AT LBL 9 IS CORRODED BETWEEN FS 409 & FS 485.00. REMOVED CORRODED CABIN FLOOR SEAT RAIL AT LBL 9 BETWEEN FS 409 TO FS485. FABRICATED, LOCATED, DRILLED & INSTALLED A NEW SERVICEABLE SEAT RAIL FROM P/N N126-2075, IAW CRJ 900 SRM 53-00-49-201-002-A01 AND CRJ900 AMM 53-00-49-400-801-A13.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,630 hrs · 15,566 cycles
CABIN FLOOR SEAT RAIL AT RBL 9 IS CORRODED FS 349.00 TO FS 485.00. REMOVED CORRODED CABIN FLOOR SEAT RAIL AT RBL 9 BETWEEN FS 349 TO FS 485. FABRICATED, LOCATED, DRILLED AND REINSTALLED A NEW SERVICEABLE SEAT RAIL FROM P/N N126-2075, IAW CRJ 900 SRM 53-00-49-201-002-A01.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,630 hrs · 15,566 cycles
PAX FLOOR SEAT TRACK BETWEEN FS 485.00 AND FS 581 RBL 9 IS CORRODED. FABRICATED SEAT TRACK P/N: SH690-33407-1 FROM EXT 20276-288-0-0A, IAW MHIRJ REO 670-53-00-589 REV A DATED 2020-07-14. REPAIR B REWORKED AND INSTALLED NEW FABRICATED SEAT TRACK, IAW MHIRJ REO 670-53-00-589 REV A DATED 2020-07-14. REPAIR B AT RBL 9 FS 581 FROM 485.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,630 hrs · 15,566 cycles
PAX FLOOR SEAT TRACK BETWEEN FS 581.00 AND FS 661+32 RBL 9 IS CORRODED. FABBED SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-589.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,630 hrs · 15,566 cycles
PAX FLOOR SEAT TRACK BETWEEN FS 581.00 AND FS 661+32 LBL 9 IS CORRODED. FABBED SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-589. .
Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,630 hrs · 15,566 cycles
FLOOR SEAT TRACK CORRODED AT LBL 9 BETWEEN FS 847+51 AND FS 977. FAB NEW SEAT TRACK AND INSTALLED, IAW BOMBARDIER GREO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 672-836) · airframe 19,630 hrs · 15,566 cycles
FLOOR SEAT TRACK AT RBL 9 CORRODED BETWEEN FS 672 TO FS 836.50. FABRICATED SEAT TRACK P/N BA690-41125-26 FROM EXT, MATERIAL 20276-288-0-0A PO W5158, IAW MHIRJ REO 690-53-00-445 REV DATED 2020-09-14. REMOVED, INSTALLED, & FABRICATED TRACK AT RBL 9 BETWEEN FS 672-836.5, IAW CRJ 900 AMM 53-00-49-000/400-801-A13.
Part: SEAT TRACK — CORRODED (BS 661-672) · airframe 19,630 hrs · 15,566 cycles
PAX FLOOR SEAT TRACK BETWEEN FS 661+32 & FS 672.00 RBL 9 IS CORRODED. FABBED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343.
Part: PLATE — DAMAGED (BS 501) · airframe 19,630 hrs · 15,566 cycles
FWD CARGO CEILING ANCHORING BRACKET FOR PANEL 151KLC HAS HOLES DRILLED INTO IT AT FS 501 AND APPROXIMATELY LBL 18. REPAIRED DAMAGE IN CROSSBEAM AT FS 501 LBL 18, IAW ENDEAVOR AIR EA CRJ 953-10861 REV A DATED 09/14/20. REPLACED 2 EA ANCHORING BRACKETS FOR PANEL 151KLC, IAW CRJ 900 SRM 51-42-06-001-001-A01.
Part: CROSSBEAM — DAMAGED (BS 469) · airframe 19,630 hrs · 15,566 cycles
DAMAGE FOUND IN CROSS BEAM BETWEEN LBL 9 & LBL 27 AT FS 469. DAMAGE FOUND IN CROSS BEAM BETWEEN LBL 9 & LBL 27 AT FS 469. ENDEAVOR AIR EA CRJ953-10837 REV IR DATED 09/15/20. FABRICATED AND INSTALLED A NEW NUTPLATE STRAP, IAW CRJ 900 SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,630 hrs · 15,566 cycles
RT SIDE SEAT RAIL LOCATED BETWEEN FS 785-FS 847+16 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED RT SIDE SEAT RAIL FS 785-FS 847+16, IAW CRJ 900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-00-910-801 AND AMM 53-00-49-600-801-A07.
Part: ANGLE — CRACKED (BS 280) · airframe 19,630 hrs · 15,566 cycles
FOUND INDICATION ON RT OUTBOARD ANGLE FS 280 APPROXIMATELY .625 LONG 100% FSA AT RADIUS FAILS NDT. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE P/N CC670-34269- 4S AT FS 280 RBL 9 OUTBOARD SIDE, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
Part: DRAIN — CORRODED (BS 319-333) · airframe 19,630 hrs · 15,566 cycles
INTERCOSTAL CORRODED AT STR 21L BETWEEN FS 319.70 AND FS 333.00. REMOVED 1EA CORRODED BACK UP SILL. LOCATED, DRILLED, AND INSTALLED 1EA NEW BAUR UP SILL P/N SH670-31822-1, IAW CRJ 900 SRM 51-40-06-001-001- A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001- A01 AT STR 21L BETWEEN FS 319-FS 333.
Part: STIFFENER — CRACKED (ASSIST MOTOR) · airframe 19,630 hrs · 15,566 cycles
PAX DOOR ASSIST MOTOR LOWER BRACKET CRACKED. REMOVED CRACKED BRACKET LOCATED, DRILLED & INSTALLED 1 EA NEW PAX DOOR ASSIST MOTOR LOWER BRACKET, IAW CRJ 900 SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, P/N 601R317745-7.
Part: RESISTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,629 hrs · 15,565 cycles
LH OVERWING FWD EMERGENCY LIGHT INOPERATIVE. R & R THE DIODE/RESISTOR IAW CMM 25-28-62 AND WM 91-11-00. OPS CHECKED GOOD.
2019
Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 19,147 hrs · 15,192 cycles
NW STEERING INOP ON T/O FROM STL. RESET SYS IAW CRJ 900AMM 32-51-00 NO DEFECTS NOTED AT THIS TIME.
Part: PRESSURE SWITCH — FAILED (HYD PUMP) · airframe 19,147 hrs · 15,192 cycles
NW STEERING INOP ON T/O FROM EWR. R/R # 3 HYDRAULIC SYSTEM PUMP PRESSURE SWITCH MT 129 IAW CRJ 900 AMM 29-34-01 PERFORMED OPS CHECK OF NOSEWHEEL STEERING SYSTEM IAW CRJ 900 AMM 32-51-00 OPS CHECK GOOD P/N ON/OFF 967008-1 S/N OFF 5274 S/N ON HYD13250
2018
Part: DRAG ANGLE — CRACKED (PAX DOOR STAIR) · airframe 16,879 hrs · 13,315 cycles
FOUND CRACK AT PAX DOOR STAIR AFT DRAG ANGLE, LOCATED NEAR THE PULLEY MOUNT BRACKET. REPAIRED CRACK AT PAX DOOR STAIR AFT DRAG ANGLE IAW CRJ900 SRM 52-11-04
Part: PLACARD — MISSING (PAX DOOR) · airframe 16,191 hrs · 12,758 cycles
PAX DOOR EMERGENCY EXIT PLACARD MISSING.
2017
Part: HOOK AND LOOP — DEFECTIVE (EMERGENCY EXIT) · airframe 14,534 hrs · 11,394 cycles
EMERGENCY EXIT ROW HOOK ANF LOOP, LEFT SIDE, WILL NOT STICK. REATTACHED ESCAPE ROPE COVER IAW AMM 52-21-03 OPS CHECK GOOD.
Part: HINGE — GOUGED (RT AILERON) · airframe 14,495 hrs · 11,366 cycles
DAMAGE FOUND ON THE RT AILERON HINGE NR 2. REPAIRED THE AILERON CENTER HINGE IAW REO 690-57-61-143, REV -, AND SRM 51-24-11.
Part: FRAME — CRACKED (BS 280) · airframe 14,495 hrs · 11,366 cycles
LT FRAME BS 280 LOWER WEB CORRODED AND CRACKED. CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-11-594, REV A, SRM 51-42-06, 51-21-11, 51-25-06, AND 51-25-16.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 14,495 hrs · 11,366 cycles
LT AND RT FRAME BS 280 CROSSBEAM CRACKED. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-11, 51-42-13, 51-42-06, 51-21-11, 51-25-16, 51-42-21 AND AMM 20-70-00.
Part: WEB — CRACKED (E/E BAY) · airframe 14,495 hrs · 11,366 cycles
FORWARD EQUIPMENT BAY RT FLOOR WEB CRACKED. REPAIRED THE FLOOR WEB IAW REO 670-53-11-509, REV.D, SRM 51-40-11, 51-21-11, 51-25-06, AND 51-25-16.
Part: MOUNT — CRACKED (ASSIST MOTOR) · airframe 14,495 hrs · 11,366 cycles
PASSENGER DOOR POWER ASSIST MOTOR MOUNT IS CRACKED. REMOVED AND REPLACED THE MOUNT IAW SRM 51-42-06, 51-40-11, AND 51-25-16.
Part: COVER — DETACHED (DOOR HANDLE) · airframe 12,875 hrs · 10,074 cycles
EMERGENCY DOOR HANDLE COVER DETACHED AT ROW 12A. SECURED OVERWING EMERGENCY DOOR HANDLE COVER IAW AMM 52-21-61.
Part: HOOK AND LOOP — DETACHED (HANDLE) · airframe 12,697 hrs · 9,933 cycles
EMERGENCY HANDLE COVER HOOK AND LOOP WILL NOT STAY ATTACHED. ATTACHED THE HOOK AND LOOP AS REQ IAW AMM 51-23-00.
2016
Part: VENT — LACK OF LUBE (PAX DOOR) · airframe 10,151 hrs · 7,955 cycles
LOUD NOISE FROM PAX DOOR 2ND ATTEMPT. PERFORMED ZONAL INSPECTION & OPERATIONS CHECK OF PAX DOOR IAW AMM 52-11-00. PRESSURIZED ACFT FOR MX IAW AMM 21-31-00. PERFORMED INSPECTION OF ACFT & FOUND TO BE SAFE FOR A ONE TIME FERRY FLIGHT. INSPECTION FOUND THE EIGHT VENT HOLES NOT TO BE OILED. PERFORMED VENT HOLES OILED IAW AMM 52-11-07. COMPLIED WITH LEAK TEST OF PRESS IAW AMM 52-00-00 & 21-31-00, NO DEFECTS NOTED.
Part: CABLE — UNSERVICEABLE (PAX DOOR) · airframe 10,151 hrs · 7,955 cycles
LOUD NOISE & VIBRATION FROM PAX DOOR IN FLIGHT. INSPECTED PAX DOOR IAW AM 05-21-00 & FOUND PAX DOOR CABLE UNSERVICEABLE. R & R PAX DOOR CABLE & PERFORMED OPERATIONS CHECK IAW AMM 52-11-15.
2015
Part: DOOR SEAL — UNKNOWN (CABIN DOOR) · airframe 10,115 hrs · 7,925 cycles
LOUD NOISE & VIBRATION COMING FROM MAIN CABIN DOOR AREA. R & R MAIN CABIN DOOR SEAL IAW 52-11-07. PERFORMED LEAK TEST OF THE PAX DOOR.
Part: DOOR SEAL — DAMAGED (PAX DOOR) · airframe 10,115 hrs · 7,925 cycles
PASSENGER DOOR MAKING A LOUD NOISE & VIBRATION IN FLIGHT. REPAIRED PAX DOOR SEAL IAW SRM 52-11-07. PERFORMED PRESSURIZATION OF AC IAW AMM 21-31-00. OPERATIONS CHECKED GOOD, NO LEAKS NOTED.
Part: DOOR — DIRTY (CABIN) · airframe 10,112 hrs · 7,923 cycles
LOUD SQUEAL FROM PAX DOOR. CLEANED & LUBRICATED PAX DOOR IAW AMM 12-20-52.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,639 hrs · 7,560 cycles
PASSENGER DOOR OUTER HANDLE CAUTION MSG. DEFERRED PAX DOOR INDICATION ON DMI 33920571.
Part: SENSOR — OBSTRUCTED (PAX DOOR) · airframe 9,627 hrs · 7,553 cycles
PASSENGER DOOR WARNING INDICATING NOT CLOSED OR LOCKED, RED. INSPECTED & REMOVED DEBRIS FROM PX107. PERFORMED OPERATIONS CHECK OF THE PAX DOOR WARNING SYS IAW AMM 52-70-00, NO FURTHER DEFECT NOTED.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 9,177 hrs · 7,226 cycles
MID CABIN EMERGENCY LIGHT INOPERATIVE. SEATED CONNECTOR ON CEILING PANEL 252 LLC. OPERATIONS CHECKED GOOD IAW AMM 53-51-00. NO DEFECTS NOTED.