# Service difficulty reports: N355QS, cancelled Aug 21, 2013 A list on [N355QS, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N355QS-2013-08-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2003F00246](https://openairdocs.org/sdr/2003F00246.md): Line · cracked · Nov 6, 2002 · N355QS · Boeing 72721 · Hydraulic System, Main > IN LEVEL CRUISE FLIGHT FROM DAY TO PHX, COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. PERFORMED ALL RYAN 'A' SYSTEM HYDRAULIC LOSS CHECKLIST. EMERGENCY DECLARED. AIRCRAFT LANDED PHX WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER RETURN LINE. (M) - [SDR 2001F00426](https://openairdocs.org/sdr/2001F00426.md): Skin · corroded · Sep 1, 2001 · N355QS · Boeing 72721 · Fuselage Main, Plate/Skin > FOUND FUSELAGE UPPER LOBE INTERIOR WING CENTER SECTION UPPER SKIN HAS CORROSION AT RBL 24-45.5 BETWEEN STATION 740 AND 870. ACCOMPLISHED WING CENTER SECTION UPPER SKIN CORROSION REPAIR AT STATION 752 BETWEEN STRINGER 20C AND STRINGER 21C IAW AVHM-2430RO-1 REV - [SDR 2001F00425](https://openairdocs.org/sdr/2001F00425.md): Floorbeam · corroded · Aug 7, 2001 · N355QS · Boeing 72721 · Fuselage Main, Floor Beam > FOUND BS 620 FLOORBEAM CORRODED ON UPPER CAP AT RBL 50. INSTALLED FLOORBEAM REPAIR AT BS 620 UPPER CAP AT RBL 50 IAW SRM 53-10-8 FIG 3. (M) - [SDR 2001F00424](https://openairdocs.org/sdr/2001F00424.md): Spar · corroded · Aug 2, 2001 · N355QS · Boeing 72721 · Wing Spar > CENTER TANK UPPER SKIN AT REAR SPAR BS 870 HAS CORRODED AREAS FROM LBL 40 TO RBL 40. ACCOMPLISHED WING CENTER SECTION AFT SPAR UPPER CHORD AND SKIN REPAIR AT RBL 24 IAW AVHM-246RO-1 REV IR. (M) - [SDR 2001F00427](https://openairdocs.org/sdr/2001F00427.md): Floorbeam · damaged · Jul 26, 2001 · N355QS · Boeing 72721 · Fuselage Main, Floor Beam > FOUND CABIN FLOORBEAM BS 344 HAS EXCESS OF OVERSIZE HOLES ON UPPER CAP FROM LBL 62 INCHES TO RBL 62 INCHES. REPLACED SECTION OF CABIN FLOORBEAM UPPER T-CAP AT BS 344 IAW SRM 53-10-8. (M) - [SDR 2001F00404](https://openairdocs.org/sdr/2001F00404.md): Spar · corroded · Jul 26, 2001 · N355QS · Boeing 72721 · Wing Spar > WING CENTER SECTION INTERNAL AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 22L DUE TO CORROSION. INSTALLED WING CENTER SECTION AFT SPAR WEB REPAIR AT STATION 870 BETWEEN LBL 17.2 AND LBL 25.9 IAW AVITAS ENGINEERING REPAIR ORDER AVHM-237RO-1 REV 1R DATED - [SDR 2001F00408](https://openairdocs.org/sdr/2001F00408.md): Keelbeam · cracked · Jul 25, 2001 · N355QS · Boeing 72721 · Fuselage Main, Keel > KEEL BEAM WEB CRACKED AT AFT HINGE ATTACH POINT OF SAFETY BAR NEAR BS 930, LEFT WHEEL WELL. INSTALLED KEEL BEAM WEB REPAIR AT AFT HINGE ATTACH POINT OF SAFETY BAR NEAR BS 930 LEFT WHEEL WELL IAW SRM 51-40-2. (M) - [SDR 2001F00407](https://openairdocs.org/sdr/2001F00407.md): Door Frame · cracked · Jul 20, 2001 · N355QS · Boeing 72721 · Passenger/Crew Doors > MAIN ENTRY DOOR INNER SURFACE AT UPPER TORQUE TUBE AFT AREA, FOUND FRAME AND WEB WITH HEAVY CRACK DAMAGES. INSTALLED REPAIR ON MAIN ENTRY DOOR INNER SURFACE AT UPPER TORQUE TUBE AFT AREA OF FRAME IAW AVITAS ENGINEERING ORDER AVHS 241-R0-1 REV 1. (M) - [SDR 2001F00414](https://openairdocs.org/sdr/2001F00414.md): Rub Strip · bulged · Jul 18, 2001 · N355QS · Boeing 72721 · Vertical Stabilizer > VERTICAL STABILIZER, LEFT UPPER SIDE RUB STRIP, SHOWS BULGES IN SEVERAL AREAS. REPAIRED VERTICAL FIN TRACK OUTBOARD LEFT SIDE IAW SRM 51-30-2 AND AVHM-245RO-1 REVISION R1. (M) - [SDR 2001F00392](https://openairdocs.org/sdr/2001F00392.md): Frame · dented · Jul 12, 2001 · N355QS · Boeing 72721 · Fuselage Main, Frame > LEFT CABIN FRAME BS 380 HAS DENT AT INBOARD FLANGE JUST ABOVE FLOOR. INSTALLED DOUBLER REPAIR AT LEFT CABIN FRAME BS 380 INBOARD FLANGE JUST ABOVE FLOOR IAW WITH SRM 51-40-3. (M) - [SDR 2001F00423](https://openairdocs.org/sdr/2001F00423.md): Spar · corroded · Jul 11, 2001 · N355QS · Boeing 72721 · Wing Spar > WING CENTER SECTION FRONT SPAR BS 740 LOWER CHORD OUTBOARD OF VERTICAL STRINGER F5 HAS TWO RIVETS POPPED OUT AND SKIN BULGING. INSTALLED REPAIR ANGLES AND STRAPS WING CENTER SECTION FRONT SPAR LOWER CHORD AT STATION 740 RBL 42 THROUGH 48.43 IAW AVHM 238R0-1. - [SDR 2001F00422](https://openairdocs.org/sdr/2001F00422.md): Spar · corroded · Jul 11, 2001 · N355QS · Boeing 72721 · Wing Spar > WING CENTER SECTION, INTERNAL, AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 45 R. INSTALLED DOUBLER REPAIR AT AFT WEB, STATION BS 870, RBL 50.9 IAW AVHM-23RO-1 REVISION R1. (M) - [SDR 2001F00406](https://openairdocs.org/sdr/2001F00406.md): Attach Angle · cracked · Jul 1, 2001 · N355QS · Boeing 72721 · Fuselage Miscellaneous Structure > FUSELAGE AIRCRAFT BAY AREA FS 758 LBL 7 BELLY FAIRING SUPPORT BRACKET ATTACH ANGLE IS CRACKED. REPLACED BELLY FAIRING SUPPORT BRACKET ATTACH ANGLE AT FUSELAGE, AIRCRAFT BAY FS 758 LBL 7 PER AVIATS ENGINEERING DRAWING AVHM 232D-1. (M) - [SDR 2001F00395](https://openairdocs.org/sdr/2001F00395.md): Frame · cracked · Jun 3, 2001 · N355QS · Boeing 72721 · Cargo/Baggage Doors > MAIN CARGO DOOR UPPER FRAME LOWER CHORD BS 581 SHOWS CRACK AT FRAME END, VIEW FROM LIGHTING HOLE. INSTALLED ANGLE REPAIR AT MAIN CARGO DOOR FRAME LOWER CHORD BS 584 IAW AVBORNE DWG N355QS-2 AND SIE 8110-3. (M) - [SDR 2001F00394](https://openairdocs.org/sdr/2001F00394.md): Structure · corroded · Jun 3, 2001 · N355QS · Boeing 72721 · Fuselage Main, Structure > SNOW WHITE POWDER AND CORROSION AT BS 481 FROM STRINGER 4L TO 4R. REPAIRED BS 481 FROM STRINGER 4L AND 4R IAW AVBORNE DWG NR 355QS AND SIE 8110-3. (M) - [SDR 2001F00393](https://openairdocs.org/sdr/2001F00393.md): Structure · corroded · Jun 3, 2001 · N355QS · Boeing 72721 · Fuselage Main, Structure > FOUND COCKPIT BS 259 BETWEEN STRINGER 6L AND 7L HAS WHITE POWER AROUND DOUBLER EDGE. INSTALLED DOUBLER REPAIR IAW B727 SB 727-53-0084 AND DRAWING NR 69-62161 AT BS 259 BTW STRINGER 6L AND 7L BTW STRINGER 6L AND 7L. (M) - [SDR 20010112SG063](https://openairdocs.org/sdr/20010112SG063.md): Uplock Switch · damaged · Nov 4, 2000 · N355QS · Boeing 72721 · Landing Gear Retraction/Extension System > FLT 580 - EN ROUTE TO DSM, NOSE GEAR LIGHT FAILED TO ILLUMINATE WHEN THE GEAR WAS EXTENDED. GEAR WARNING HORN SOUNDED CONTINUOUSLY. AIRCRAFT LANDED DSM SAFELY AND WITHOUT INCIDENT. FOUND GROUND WIRE ON NOSE GEAR LOCK SWITCH BROKEN. REPAIRED GROUND WIRE AND - [SDR 20001128AP011](https://openairdocs.org/sdr/20001128AP011.md): Engine · vibration · Jul 26, 2000 · N355QS · Boeing 72721 · Engine (Turbine/Turboprop) > FLT 705 - BWI-IND - IN CRUISE AT FLIGHT LEVEL 310, EXPERIENCED SUDDEN VIBRATION. ALL ENGINE GAUGES AND PARAMETERS APPEARED NORMAL, BUT BY POWERING BACK ON NR 2 THE VIBRATION. ALL ENGINE GAUGES AND PARAMETERS APPEARED NORMAL, BUT BY POWER BACK ON NR 2 THE VIB - [SDR 20001004AP007](https://openairdocs.org/sdr/20001004AP007.md): Bulb · failed · Jun 17, 2000 · N355QS · Boeing 72721 · Detection System > FLT 749 - SLC - NR 2 CARGO SMOKE DETECTOR WILL NOT TEST. GAINED ACCESS TO NR 2 SMOKE DETECTOR UNIT, RELAMPED TEST AND BEAM BULBS. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N355QS' AND deregistration_id = 'N355QS-2013-08-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N355QS-2013-08-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.