N153PQ
Service difficulty reports · 225
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N153PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N153PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR REXA2019081328172Stringer · corroded"LATE FINDING: CORROSION ON INTERNAL STGR 22R BTW FS333 TO FS349. CORROSION LEVEL 2 ON INTERNAL STGR 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT E/E WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR REXA2019081301169Angle · corroded"LATE FINDING: CORROSION ON ANGLE STGR 21R BTW FS364 TO FS379. AMAGE ANGLE ON STGR 21RH BTW FS 364 TO FS 379 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6. STGR 21RH WAS MEASURED AS FOLLOW: ORIGINAL THICKNESS 0.080¨, REMAINING THICKNESS 0.038¨ IT WASSDR REXA2019081281154Support Angle · corrodedCORROSION ON PROTECTOR PLATE SUPPORTS AND ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE. SUPPORTS AND ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE, WERE REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.SDR REXA2019081281152Doubler · corroded"INITIAL INSPECTION: CORROSION ON INTERNAL PRODUCTION DOUBLER IN BS 295 TO 310 BETWEEN STGR 26LH TO 26RH IN THE E/E COMPARTMENT. INTERNAL PRODUCTION DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-20-001-001-A01.SDR REXA2019081321168Splice · corrodedCORROSION ON STRINGER SPLICE 21R AND BS 333. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01.
"SDR REXA2019081371166Stringer · corrodedCORROSION ON INTERNAL STGR 21R BTW FS394 TO FS409. STRINGER 21R WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR REXA2019081371165Stringer Splice · corrodedCORROSION ON STGR SPLICE 26L, BS 333 AT MAIN AVIONICS COMPARTMENT. REMOVED THE STRINGER SPLICE 26L, A NEW SPLICE WAS INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.SDR REXA2019081271160Intercostal · corrodedCORROSION ON INTERCOSTAL E/E COMPARTMENT BTW FS=310/319 AND STGR 20R .INTERCOSTAL E/E COMPARTMENT BTW FS=310/319 AND STGR 20R WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01-AND SRM 51-42-21-001-001-A01.SDR REXA2019081271151Support Angle · corrodedCORROSION ON INTERNAL FUSELAGE STRUCTURE AT SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB. SUPPORT ON SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL (195AB) WAS REPLACED IAW SRM 51-42-10-001-001-A01 AND INTERNAL FUSELAGE STRUCTURE AT SETTLEMENT AREASDR REXA2019081361167Stringer · corrodedCORROSION ON INTERNAL STRINGER 21R BETWEEN BS 364 - 379. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
"SDR REXA2019081261155Stringer · corroded"INITIAL INSPECTION: CORROSION ON INTERNAL STGR 18R BTW FS394 TO FS409. THE STRINGER WAS REPAIRED IAW SRM 53-00-03-201-001-A02, FIG.53-00-03-995-807,SOLUTION II.SDR REXA2019081324171Stringer Splice · corroded"LATE FINDING: CORROSION ON SPLICE 22R BTW FS333 TO FS349 (E/E). CORROSION ON SPLICE 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT, NEW SPLICE 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT (E/E) WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 SDR REXA2019081301164Stringer · corrodedCORROSION ON STRINGER SPLICE 27, BS 333 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE NBR 27 STA FS= 333 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.SDR REXA2019081201162Intercostal · corrodedCORROSION ON INTERCOSTALS AT E/E COMPARTMENT BTW FS=310/349 AND STGR 21L. INTERCOSTALS AT E/E COMPARTMENT BTW FS=310/349 AND STGR 21 LH (2 E/AS) WERE REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01.SDR REXA2019081201161Stringer · corrodedCORROSION ON STGR 20R AT E/E COMPARTMENT BTW FS=280/295. STRINGER 20 RH BTW FS=280 AND FS=315 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01.
"SDR REXA201901291158Canister · crackedCRACK IN CANISTER WELDED NO. 3 ASSY RIGHT OUTER WINGBOX FUEL TANK. CRACKED CANISTER WELDED NR 3 ASSY RIGHT OUTER WINGBOX FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. -- .SDR REXA2019081291156Canister · crackedCRACK IN CANISTER WELDED NO. 3 ASSY LEFT OUTER WINGBOX FUEL TANK (SM). CANISTER WELDED THE NR 3 ASSY LEFT OUTER WINGBOX FUEL TANK WAS REPAIRED AND ATTENDED PER REO 670-57-42-577 REV.--SDR REXA201908129144Stringer Splice · corrodedINITIAL INSPECTION:CORROSION ON STGR SPLICE NBR 26 RH STA FS= 333 AT MAIN AVIONICS COMPARTMENT. STGR SPLICE 26 RH STA FS= 333 AT MAIN AVIONICS COMPARTMENT WAS MEASURED AS FOLLOW: ORIGINAL THICKNESS 0.063¨, REMAINING THICKNESS 0.055¨ IT´S OUT OF LIMITS, REPLASDR REXA2019081281159Canister · crackedCRACK IN BRACKET SUPPORT OF CANISTER WELDED NO. 1 ASSY RIGHT OUTER WINGBOX FUEL TANK. NEW BRACKET SUPPORT OF CANISTER WELDED NR 1 ASSY RIGHT OUTER WINGBOX FUEL TANK WAS DRILLED PER SRM 51-40-11-001-001-A01 AND NEW BRACKET SUPPORT OF CANISTER WELDED NR 1 ASSSDR REXA2019081281153Support Fitting · corrodedCORROSION ON FLOOR STRUCTURE GALLEY FITTING SUPPORT BTW FS 280/295 AND RBL 17 IN REF EO R53520 STEP 7. THE FITTING WAS REPLACED IAW SRM 51-42-21-001-001-A01.SDR REXA2019081271150Structure · crackedCRACK ON BOX OF THE EXTERNAL POWER RECEPTACLE AT THE FWD FUSELAGE. EXTERNAL POWER BOX WAS FABRICATED PER EA NO: CRJ953-09257 REV.IR ,AND REPAIR PARTS, EXTERNAL POWER BOX WAS INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01SDR REXA201906170886Battery Pack · inoperativeBOTH (LEFT&RIGHT) AFT OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R AFT EPSU BATTERY CHARGER ASSEMBLY P/N ON/OFF 11-0049 S/N ON 22480S/N OFF 22621 IAW CRJ900 AMM 35-51-17. R+R EPSU BATTERY PACK PS38 P/NON AD-2013-1A S/N ON 178193 P/N OFF 2013-1ASMI S/NSDR REXA2018083000761Battery Pack · dischargedDURING OPERATIONAL CHECK OF EMERGENCY LIGHTS NOTED INTERMITTANT ILLUMINATION OF EXIT LIGHTS AT OVERWING EXITS. REMOVED & REPLACED EMERGENCY BATTERY PACK AT POSITION PS43, IAW AMM CH 33-51-17. OPS CHECK GOOD.SDR REXA2018062200526Life Vest · missingUPDATE ON PROBLEM DESCRIPTION. DURING EE-900 INSPECTION NOTED SEAT 1C MISSING LIFE VEST. INSTALLED LIFE VEST BOX STRAP ON PASS SEAT 1C IAW TS 005235B.SDR REXA201805010326Oxygen Mask · brokenFIRST OFFICER`S OXYGEN MASK WAS BROKEN. R & R THE OXYGEN MASK.IAW AMM 35-11-12, OPS CHECKED GOOD IAW AMM 35-10-00. OK FOR SERVICE.SDR REXA2018041900302Strut · dischargedGEAR DISAGREE, NOSE WHEEL STAYED DOWN WHEN GEAR RETRACTED. INSPECTED THE NOSE STRUT. SERVICED THE NOSE STRUT WITH OIL AND NITROGEN IAW AMM 12-12-32, JACKED THE AIRCRAFT IAW 07-12-03, PERFORMED A GEAR RETRACTION AND EXTENTION, NO FAULTS NOTED. AIRCRAFT OKASDR ASOA201612241377Light · inoperativeEMERGENCY LIGHT OVERWING RT SIDE INOPERATIVE. REMOVED & REPLACED RT SIDE OVERWING AFT LIGHT ASSY IAW AMM 33-51-15 OPS CHECKED GOOD.SDR ASOA201612241376Connector · disconnectedLEFT WING AFT EMERGENCY LIGHT INOPERATIVE. RECONECTED CONNECTOR PLUG BEHIND SIDE WALL PANEL 16AB AND REMOVED & REPLACED LIGHT ASSY IAW AMM 33-51-15. AND REMOVED & REPLACED PCB5 RELAY K135 IAW AMM 24-06-01. OP CHECKED GOOD.SDR ASOA201612141358Bulb · burned outRIGHT WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-15. OPS CHECKED GOOD.SDR ASOA2016080915231Charger · inoperativeEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-11. REMOVED AND REPLACED THE BATTERY CHARGER NR 1 IN AVIONICS COMPARTMENT IAW AMM 33-51-17.SDR ASOA2016080515191Sign · missingEXIT SIGN IN THE GALLEY IS MISSING. REPLACED THE SIGN IAW AMM 33-51-05.SDR ASOA2016051814840Wire · brokenRT WING FWD EMERGENCY EXIT LIGHT INOPERATIVE. EXTERIOR EMERGENCY LIGHTS, FORWARD OVERWING EMERGENCY LIGHT ON EACH SIDE. TROUBLESHOOT RT WING FWD EMERGENCY EXIT LIGHT IAW FIM 33-51-00 AND WIRING DIAGRAM 33-51-01. FOUND WIRE AT P396 BROKEN REPAIR WIRE IAW ESSDR ASOA2016051714837Wire · damagedBATTERY HOUSING WIRING DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14. AIPC REF 25-61-14, FIG. 1K, ITEM 5.SDR ASOA2016051714836Battery Pack · inoperativeRT REAR EXIT EMERGENCY LIGHT INOPERATIVE. R & R EXIT EMERGENCY LIGHT ASSY, RT FWD, IAW AMM 33-51-15. R & R ESPU BATTERY PACK NR 3 IAW AMM 33-51-17.SDR ASOA2016041214698Retainer · bentCENTER CARGO BAY DOOR SEAL RETAINER BENT AT FORWARD LOWER CORNER. PERFORMED PERMANENT REPAIR TO FORWARD LOWER CORNER OF CENTER CARGO BAY SEAL RETAINER IAW EC/TC REO 690-52-35-013. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.SDR ASOA2016032614676Support Fitting · damagedCOMPLY WITH PERMANENT REPAIR OF H/S BELLCRANK SUPPORT FITTING INSTALLATION LT SIDE, RT SIDE ATTACHMENT FASTENERS IAW REO 69055-11-069. COMPLIED WITH PERMANENT REPAIR OF LT SIDE, RT SIDE BELLCRANK SUPPORT FITTINGS IAW EC/TC REO 690-55-11-094. COMPLIED WITH ECSDR ASOA2016030914620Intercostal · corrodedINTERCOSTAL BETWEEN FS 349 TO FS 364 AT CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 DWG SH670-32075 AT STR 27R RT WING FS 349 & 364.SDR ASOA2016030714623Floorbeam · corrodedDURING REMOVAL OF BS 280 FLOORBEAM ANGLE CORRODED AT LBL 9 FWD SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 690-53-11-859, STEPS 1-7, EM12174 3/10/16 (PB) M/A: 4.SDR ASOA2016030714622Stringer Splice · corrodedWHILE ADDRESSING CORROSION ON STR 25R DISCOVERED CORROSION AROUND FASTENERS ON STR SPLICE 26R BETWEEN FS 319-333. BLENDED CORROSION REF SRM 51-21-06-001001-A01 & SRM 51-42-06-001-001-A01. DAMAGE EXCEEDS ALLOWABLE LIMITS. R & R STRINGER SPLICE IAW SRM 51-42-SDR ASOA2016030314621Floorbeam · corrodedFLOORBEAM ANGLE AT FWD SIDE OF BS 280 FLOORBEAM HAS CORROSION. REMOVED FLOORBEAM ANGLE AT FWD SIDE OF BS 280 IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-12-001-001-A01. LOCATED AND DRILLED NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01. LOCATED AND DRILLESDR ASOA2016030314619Angle · corrodedPAX DOOR SILL ANGLE HAS CORROSION. REMOVED PAX DOOR SILL MID CAP ANGEL IAW SRM 51-41-00-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW MID CAP ANGLE IAW SRM 51-42-06-001-001 A01. REMOVED PAX DOOR SILL LOWER ANGLE IAW 51-42-06-001-001 A01. LOCATED AND DRILSDR ASOA2016030314618Door Sill · corrodedFLOOR SILL FWD OF SERVICE DOOR IS CORRODED. FLOOR SILL FWD AT SERVICE DOOR CORROSION IS OUT LIMITS. REMOVED FWD OF SERVICE DOOR FLOOR SILL IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICABLE SILL ANGLE AD PARTIALLY INSTALLED SILL BETWEEN SDR ASOA2016030314569Angle · corrodedANGLE CORRODED AT RBL 9, FS 333.00. R & R IAW SRM 51-42-06-001-001-A01.SDR ASOA2016030314568Seat Track · corrodedSEAT TRACK BS 785.15 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000/900-801-A07.SDR ASOA2016030314567Seat Track · corrodedSEAT TRACK BS 752.50 CORRODED. R & R IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A01.SDR ASOA2016030314566Seat Track · corrodedSEAT BS FS 720.85 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A07.SDR ASOA2016030314565Seat Track · corrodedLT SIDE SEAT TRACK AT FS 785.15 CORRODED. R & R COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.SDR ASOA2016030314564Seat Track · corrodedLT SIDE SEAT TRACKS AT FS 752.50 CORRODED. R & R SEAT TRACK IAW SRM 51-41-00-001-001-A01.SDR ASOA2016030314563Seat Track · corrodedSEAT TRACK AT BS 720.85 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.SDR ASOA2016030314562Seat Track · corrodedLEFT SIDE SEAT TRACK AT BS 597 - 661 AT STRINGER 15L. R & R LT SIDE SEAT TRACK AT FS 597.00 TO 661.00 IAW AMM 53-00-49-000-801A-07 AND 53-00-49-400-801-A07.
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