N2824W
Registered owner: BROWN LOGISTICS LLC, WA (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.
34 reports on file, 1995-03-09 – 1995-12-01.
Part: BATTERY PACK — DISCHARGED (CABIN)
ON LAYOVER, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT OVERWING EMERGENCY EXITS LT SIDE. REPLACED M1090 BATTERY PACK, EMERGENCY LIGHTS OPS NORMAL.
Part: FITTING — CORRODED (NR 4 FLAP TRACK)
FOUND AT HMV, FRETTING CORROSION ON I/B FACE OF LT MLG PORK CHOP FITTING AT FLAP TRACK ATTACH HOLE. REPAIRED PER MM 57-42-0 PG 814.
Part: BUSHING — LOOSE (NR 4 FLAP TRACK)
AT HMV, FOUND BUSHING LOOSE IN LT MLG PORK CHOP FTG IN AFT HOLE FOR NR 4 FLAP TRACK. REPAIRED AND INSTALLED NEW BUSHING PER MM 57-42-0.
Part: DOUBLER — CRACKED (BS 938)
THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK WAS FOUND WITH A PREVIOUS MODIFICATION DOUBLER INSTALLED FOR A CRACK AT LBL 55 AND STA 938. THE PREVIOUS DOUBLER WILL BE REMOVED AND A NEW DOUBLER INSTALLED PER REVISION 4 OF THE SERVICE BULLETIN E0 4.61537-3AD, S/B 727-53-0149. THE NEW DOUBLER WILL BE EXTENDED TO PICK UP ANY FASTENER LOCATIONS INSTALLED BY THE ORIGINAL REPAIR. ACCOMPLISHED REPAIRS PER DL ERA 302615-14AD.
Part: RIB — CRACKED (NR 4 LE SLAT)
AT HMV, NR 4 SLAT RIB NR 18 CRACKED. REPAIRED PER MM 57-54-00.
Part: STRINGER — CRACKED (NR 1 ENG COWL)
DURING A HANGAR INSPECTION, A CRACK WAS DISCOVERED IN THE FWD STRINGER OF THE NR 1 ENGINE LWR COWL. A REPAIR WAS INSTALLED PER THE S.R.M. 51-40-3.
Part: SKIN — CORROSION (BS 950)
AT HMV IN ATLANTA, MTC FOUND CORROSION IN FUSELAGE SKIN AT STA 950 PLUS 10 INCHES JUST OUTBOARD OF STR 30. FINAL CUT-OUT DIMENSIONS ARE 2.75 INCHES BY 3.75 INCHES. THE SKIN IS FABRICATED FROM 2024-T3 CLAD AND HAS A NOMINAL THICKNESS OF 0.183 INCH AT THE FWD LOCATION OF THE CUT-OUT AND 0.145 INCH ALONG THE AFT EDGE OF THE CUTOUT. ER/A REPAIRED DAMAGED AREA BY INSTALLING A DOUBLER, TRIPLER, AND QUADRUPLER AND CHEM TREATING THE AREA.
Part: VENT ACCESS HOLE — MISLOCATED (WS 656.5)
DURING ACCOMPLISHMENT OF THE LT WING UPPER STRINGER 13/14 TAB ONLY REPAIR AT WS 656.5 RIB, THE VENTB OX ACCESS HOLE WAS INADVERTENTLY CUT INBD OF THE RIB INSTEAD OF OTBD. THIS REPAIR WAS BEING ACCOMPLISHED PER B727 M/M 57-13-0 FIG. 804, REPAIR FOR TAB CRACKS ONLY. THIS ER/A AUTHORIZES MIRRORING THE REPAIR TO ACCOMMODATE THE ACCESS HOLE ON THE INBD SIDE OF WS 656.5 RIB. AD 88-17-06.
Part: ANGLE — CRACKED (NR 1 LE FLAP)
NR 1 L/E FLAP ACTUATOR ATTACH ANGLE CRACKED I/B SIDE. WORKED AT HMV, REPAIRED ANGLE PER M/M 57-20-21.
Part: SKIN — CRACKED (VERT STAB)
AT HMV, FOUND VERT STABILIZER SKIN STOPPED DRILLED 3 TIMES AT RT FS 1333 AT BOTTOM OF VERT FIN. REPAIRED PER MM 55-30-0 PG 801.
Part: SUPPORT — CRACKED (RT ELEV)
RT ELEVATOR-HINGE SUPPORT FRAME CRACKED AT BOLT, INSIDE 3RD BALANCE BAY FROM O/B END, WORKED AT HMV. REPAIRED PER SRM 55-10-04, FIG 6.
Part: RIB — CRACKED (NR 5 LE SLAT)
NR 5 SLAT-RIB NR 20 CRACKED UNDER LEADING EDGE AT NUTPLATE. WORKED AT HMV. REPAIRED PER M/M 57-54-00.
Part: VENT BOX TAB — CRACKED (RT WING)
REF OPN 8602 AD HFEC INSP OF RT OUTER WING UPPER STRINGER-TO-RIB CRACK INDICATED FWD VENT BOX AFT TAB W.S. 686.5, MARKED NR 2.
Part: STRINGER — CRACKED (LT WING)
HFEC CHECKED ON STR-TO-RIB HOLES SHOWS CRACK INDICATION ON STRINGER NR 10 AND NR 14 AT W.S. 656.5. WORKED AT HMV. INSTALLED REPAIR DOUBLER PER M/M 57-13-00.
Part: HEAT SHIELD — CRACKED (NR 6 LE SLAT)
NR 6 SLAT-INTERIOR HEAT SHIELD CRACKED BETWEEN RIBS 11 AND 12. WORKED AT HMV. REPAIRED PER M/M 57-54-00, PG 804A.
Part: WEB — CRACKED (VERT STAB)
AT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.
Part: WEB — CRACKED (VERT STAB)
AT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.
Part: FRAME — CRACKED (FS 930)
AT HMV, FOUND FUSELAGE FRAME CRACKED AT REPAIR DOUBLER, UPPER FASTENER HOLE FS 930 RT SIDE. REPAIRED PER SRM 53-10-04 FIG 25 TYP B.
Part: VENT BOX TAB — CRACKED (WS 686)
TAB CRACKED. VENT BOX TAB CRACKED STA. 686.5 AT HOLE MARKED NR 4. WORKED AT HMV. REPAIRED TAB PER M/M 57-13-00.
Part: RIB — CRACKED (NR 4 LE SLAT)
NR 4 SLAT-RIB NR 2 CRACKED. WORKED AT HMV. REPAIRED PER M/M 57-40-00, FIG 805.
Part: WEB — CRACKED (BS 1303)
AT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 LT ABOVE S-DUCT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17.
Part: SKIN — CRACKED (NR 2 ENG INLET)
AT HMV, FOUND SKIN CRACKED NR 2 ENG INLET AT 3 O'CLOCK POS, 10 INCHES AFT OF LIP. FABRICATED AND INSTALLED NEW REPAIR PER MM 54-30-0 PG 801.
Part: SKIN — CRACKED (ACC DOOR CUTOUT)
AT HMV, FOUND .375 CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUOUT. REPAIRED PER MM 53-30-0 PG 803.
Part: STRINGER — CRACKED (VERTICAL STAB)
AT HMV, FOUND STRINGER CRACKED VERTICAL STAB INTERIOR STR 8R LOC IN 5TH BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-00 FIG 803.
Part: STRINGER — CRACKED (VERT STAB)
STRINGER CRACKED VERT STAB INTERIOR STR 8R CRACKED, LOCATED IN 3RD BAY UP FROM ACCESS HOLE. WORKED AT HMV, REPAIRED PER M/M 55-30-00.
Part: WEB — CRACKED (BS 1303)
AT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 RT SIDE ABOVE S-DUCT. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 17.
Part: WEB — CRACKED (BS 913.5)
WORKED AT HMV. PERFORM PERMANENT REPAIR, CRACK STA 913.5 LT, PER M/M 53-11-00, PG 816. REMOVED AND INSTALLED REPAIR PER M/M 53-11-00.
Part: WEB — CRACKED (BS 1223)
AT HMV, FOUND .5 INCH CRACK IN LT TORQUE BOX WEB IN 48 SECT STA 1223 AT UPPER RIVET ROW. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0 PG 833.
Part: SKIN — DENTED (FS 1148)
DEFERRED FROM NR 15. WORKED AT HMV, 6 INCHES LONG BY 2 INCHES WIDE, DENTED/SCRATCHED AREA LWR RT FUSELAGE SKIN STA 1148 BETWEEN STR 19R AND 20R. REPAIRED PER SRM 53-30-03.
Part: SPAR — CRACKED (LT TE MID FLAP)
NR 3 MID FLAP DURING HMV INSPECTION FOUND A CRACKED AFT SPAR CORD 19 INCHES FROM I/B END AND A CRACKED DOUBLER 37 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0 NRC38851 (2) AFT SPAR CORD WAS CRACKED 41 INCHES FROM O/B END. REPAIRED PER M/M 57-52-0. NRC 8852.
Part: EEL POWER SUPPLY — FAILED (CABIN)
FLOOR EMERGENCY EXIT LIGHTS INOP AFT OF ROW 26. FOUND PWR SUPPLY BAD FOR AFT EMERGENCY TRACK LIGHTING. REPLACED SAME EMERGENCY LIGHTS, NOW TEST NORMAL.
Part: WINDSHIELD — SHORTED/ARCING (RT FLT DECK)
DURING CRUISE, COPILOTS WINDSHIELD SHORTED WITH SPARKS BEING EMITTED. SHUT-OFF WINDOW HEAT, NO FURTHER ARCING. REPLACED WINDSHIELD AND CONTROLLER.
Part: WEB — CRACKED (AIR STAIR)
FOUND ON LETTER CHECK STA 1235 LT LIGHTENING HOLE DAMAGED AT 7:00 POSITION AIR STAIR VERTICAL WEB. REPAIR INSTALLED DOUBLER PER MM 53-11-0 PG 828.
Part: FLAP — CRACKED (NR 4 FORE FLAP)
FOUND ON LETTER CHECK NR 4 FORE FLAP L/E CRACKED .25 INCH ABOVE NR 7 FLAP TRACK. REPAIRED PER SRM 57-50-4 FIG 1.