N438US
Service difficulty reports · 235
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 = 'N438US' 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 = 'N438US' 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 USAA2009010290009Skin · debondedCLT Q5 MAJOR REPAIR NR 03C30257009/005 NR 1 SLAT DISBONDED ON UPPER SURFACE AT WEDGE AREA. REPAIRED NR 1 SLAT IAW B737 SRM 57-43-02 & 51-70-10.SDR USAA2009010590031Angle · crackedCLT - Q5 - MAJOR REPAIR - NR 03C20353004/002 - CRACK ON ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R. REPAIRED ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R IAW B737 SRM 51-10-02.SDR USAA2009010590034Frame · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/004 - FUSELAGE FRAME CRACKED AT BS277, S16L. REPAIRED FUSELAGE FRAME AT BS277, S16L IAW B737 SRM 53-00-07.SDR USAA2009010590033Angle · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/002 - ANGLE CRACKED FORWARD OF R1 DOOR AT BS294.5, S17L. REPLACED ANGLE FORWARD OF R1 DOOR AT BS294.5, S17L IAW B737 SRM 51-40-02.SDR USAA2009010590032Stringer Clip · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/001 - STRINGER TIE CLIP CRACKED AT BS344, S11R. REPLACED STRINGER TIE CLIP AT BS344, S11R IAW B737 SRM 51-40-02.SDR USAA2009010290006Tab · delaminatedCLT Q5 MAJOR REPAIR NR 03C40627011/002 RT AILERON TAB SEPARATED AT OTBD END. REPLACED RT AILERON TAB & INSTALLED ON US AIRWAYS TASK CARD NR 03C40627010.SDR USAA2009010590036Strap · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/007 - CRACK ON L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L. REPLACED L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L IAW B737 SRM 51-10-02.SDR USAA2009010590035Door Frame · crackedCLT - Q5 - MAJOR REPAIR - NR 03C10753006/006 - CRACK IN R1 DOOR FRAME AT BS294.5, BETWEEN S6R & S7R. REPAIRED R1 DOOR FRAME AT BS294.5, BETWEEN S6R & S7R IAW B737 SRM 51-70-11.SDR USAA2009010590028Floorbeam · corrodedCLT - Q5 - MAJOR REPAIR - NR 03C10753060/011 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS312, RBL13 & RBL30. REPAIRED FLOORBEAM AT BS312, RBL13 & RBL30 IAW B737 SRM 53-10-51.SDR USAA2008121992278Angle · crackedCLT - Q5 - MAJOR REPAIR - ANGLE CRACKED AT BS 294, BETWEEN S11R & S12R FORWARD OF R2 DOOR. REPLACED ANGLE AT BS 294, BETWEEN S11R & S12R FORWARD OF R2 DOOR IAW B737 SRM 51-10-02.SDR USAA2008121992277Frame · crackedCLT - Q5 - MAJOR REPAIR - FRAME WEB CRACKED AT BS 328, LBL 50. REPLACED FRAME WEB AT BS 328, LBL 50 IAW SRM 51-40-02.SDR USAA2008121992276Frame · crackedCLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 747, BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 747, BETWEEN S8L & S9L TYPICAL REPAIR 53-10-20E.SDR USAA2008121992275Skin · crackedCLT - Q5 - MAJOR REPAIR - NR 1 SLAT SKIN CRACKED AT RIVET HOLES AT INBOARD AUXILIARY TRACK. REPAIRED NR 1 SLAT SKIN IAW SRM 57-43-01.SDR USAA2008121992274Strap · crackedCLT - Q5 - MAJOR REPAIR - LOWER STABILIZER STRAP CRACKED AT BS 344, LBL 44. REPLACED LOWER STABILIZER STRAP AT BS 344, LBL 44 IAW SRM 51-10-02 & DRAWING 65-45834.SDR USAA2008121992273Intercostal · corrodedFILIFORM CORROSION ON INTERCOSTAL BETWEEN BS 328 TO BS 344, LBL 12. REPLACED INTERCOSTAL BETWEEN BS 328 TO BS 344, LBL 12 IAW B737 SRM 51-40-02. UPON FURTHER REVIEW BY ENGINEERING, IT HAS BEEN DETERMINED THAT THIS IS NOT CLASSIFIED AS STRUCTURE REQUIRING CPCSDR USAA2008121992272Intercostal · corrodedEXFOLIATION ON INTERCOSTAL AT BS 328, RBL 12. REPLACED INTERCOSTAL AT BS 328, RBL 12 IAW SRM 51-40-02. UPON FURTHER REVIEW BY ENGINEERING, IT HAS BEEN DETERMINED THAT THIS IS NOT CLASSIFIED AS STRUCTURE REQUIRING CPCP INSPECTION.SDR USAA2008121892269Web · crackedCLT - Q5 - MAJOR REPAIR - CRACK ON FUSELAGE WEB AT BS 277, S14R FORWARD OF R1 DOOR. REPLACED FUSELAGE WEB AT BS 277, S14R IAW SRM 51-10-02.SDR USAA2009011290065Rib · crackedNR 03-0528-8-0176/001 AND 6099288 - CRACK ON RT WING RIB LOWER CHORD WEB AT WBL 135.5. REPAIRED RT WING RIB LOWER CHORD WEB AT WBL 135.5 IAW EA NR 100777.SDR USAA2008121792254Rib · crackedCLT - Q5 - MAJOR REPAIR - RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, 7 INCHES FORWARD OF AFT SPAR AT LOWER SKIN. REPAIRED RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, IAW US AIRWAYS EA 100777.SDR USAA2008121792253Angle · crackedCLT - Q5 - MAJOR REPAIR - ANGLE CRACKED AT BS 270, S10L. REPAIRED ANGLE AT BS 270, S10L IAW BOEING DRAWING 65-17684-65.SDR USAA2009012190102Floorbeam · corrodedCLT - Q5 - MAJOR REPAIR - NR 03C10753060/005 - CORROSION ON FLOOR BEAM TEE CAP AT BS344, LBL12 TO RBL12. REPAIRED FLOOR BEAM TEE CAP AT BS 344, LBL12 TO RBL12 IAW SRM 53-10-51.SDR USAA2008121792249Skin · debondedCLT - Q5 - MAJOR REPAIR - DISBOND AREA ON NR 3 SLAT AT UPPER INBOARD EDGE. REPAIRED NR 3 SLAT IAW B737 SRM 51-70-10.SDR USAA2008121792252Vertical Beam · crackedCLT - Q5 - MAJOR REPAIR - CRACK IN VERTICAL BEAM WEB AT BS 184.0321, LBL 17, WL 233. REPAIRED VERTICAL BEAM WEB AT BS 184.0321, LBL 17, WL 233 IAW B737 SRM 53-10-08 & ENGINEERING ORDER 5312-01008.SDR USAA2008121892268Vertical Beam · crackedCLT - Q5 - MAJOR REPAIR - CRACKS IN VERTICAL BEAM WEB AT BS 179, WL 227, RBL 17. REPAIRED VERTICAL BEAM WEB AT BS 179, WL 227, RBL 17 IAW B737 SRM 53-10-08.SDR USAA2008121792251Frame · crackedCLT - Q5 - MAJOR REPAIR - FRAME CRACKED BETWEEN BS 480, S8R & S9R. REPAIRED FRAME BETWEEN BS 480, S8R & S9R IAW TYPICAL REPAIR 53-10-20E.SDR USAA2008121792250Skin · crackedCLT - Q5 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT LOWER HINGE CUTOUT OF L2 DOOR BS 947, S14L. REPAIRED FUSELAGE SKIN AT LOWER HINGE CUTOUT IAW TYPICAL REPAIR 53-60-10.SDR USAA920081981Skin · crackedCLT RON MAJOR REPAIR LOG NR 4371367 RT HORIZONTAL STABILIZER LOWER SURFACE HAS A CRACK FORWARD OF CENTER ELEVATOR BALANCE PANEL AT AFT SPAR. REPAIRED RT HORIZONTAL STABILIZER LOWER SURFACE IAW US AIRWAYS TYPICAL REPAIR NR 55-10-07 REV D.SDR USAASB08051Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD GALLEY. OPERATIONAL CHECK GOOD. (S)SDR USAASB08052Charger · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (S)SDR USA2008F00015Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD GALLEY. OPERATIONAL CHECK GOOD. (S)SDR USA2008F00014Charger · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (S)SDR USAA920080867Skin · crackedA .3125 INCH CRACK IN FUSELAGE SKIN AT CORNER OF LWR AFT SERVICE DOOR. REPAIRED IAW EA 100368.SDR USAA920080866Web · crackedPRESSURE DECK WEB HAS 1.5" CRACK AT BS 663.75, WL 208.1, LBL 30. INSTALLED DOUBLER REPAIR IAW SRM 56-60-51.SDR USAA920070866Stringer Splice · crackedCLT - MAJOR REPAIR - FPBH INSPECTION - NR 6006809, CRACKED STRINGER SPLICE, BS 348, S15L. REPLACED STRINGER SPLICE, BS 348, S15L IAW B737 SRM 51-10-02.SDR USAA200705002Skin · cracked2" CRACK FOUND AT RT HORIZ STAB LOWER SKIN CENTER OF 3" PANEL. (CLT) INSTALLED TEMPORARY DOUBLER PER TR 55-10-07 REV B.SDR USAA200705001Skin · cracked1" CRACK FOUND AT STA 727D STR 23L ON SKIN. (CLT) INSTALLED DOUBLER PER TR 53-60-03ASDR USAA07003Door Frame · gougedAFT CARGO DOOR FWD FRAME BS 797 GOUGED. REPAIRED IAW EA 98374, DEFECT SIZE: .010 INCH.SDR USAA07004Skin · crackedRIGHT FWD CORNER OF THE EXTERNAL GROUND A/C CUTOUT CRACKED. INSTALLED DOUBLER PER EA 98372, DEFECT SIZE: 1 INCH.SDR USAASB06107Pump · leakingPIT FLT1780, ON DESCENT INTO PIT FROM BOS, CREW DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL DUE TO LOW HYDRAULIC QUANTITY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED ANDSDR SB06050Check Valve · failedAFTER TAKEOFF FROM PHL, WITH LANDING GEAR SELECTED UP, CREW REPORTED THE NOSE LANDING GEAR INDICATED BOTH RED AND GREEN LIGHTS. A NOTICEABLE AIR FLOW NOISE WAS PRESENT, SUGGESTING THE NOSE LANDING GEAR WAS STILL EXTENDED. THE MAIN LANDING GEAR INDICATED UP ASDR SB06047Module · failedCLT FLT1445, DURING CLIMB-OUT FROM CLT, EN ROUTE TO MIA, THE NOSE GEAR WOULD NOT RETRACT. WITH THE GEAR HANDLE UP, CREW RECEIVED BOTH A RED AND GREEN LIGHT INDICATION. CREW EXTENDED GEAR AND RECEIVED ALL THREE GREEN LIGHTS. FLIGHT RETURNED TO FIELD IN CLSDR SB05110Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE FORWARD ENTRY AREA EMERGENCY LIGHTS WERE DIM. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA050355Spar · chippedPIT - Q4 - RUDDER L/E SPAR, .2500 INCH X .1250 INCH DEEP CHIP IN EDGE CHIP, LT L/E SPAR TAB. BLEND OUT REPAIR, HFEC INSPECTION AND VISUAL, SEALED IAW EA 79967. (K)SDR USAA050358Skin · damagedPIT - Q4 - COMP SKIN LT ELEVATOR, 2.5 INCH LENGTH X .125 INCH WIDTH, COMPOSITE DAMAGE, STA 55 AT PANEL CENTER TOP SURFACE LT ELEV. INSTALLED REPAIR PLIES IAW SRM AND EA. (K)SDR USAA050333Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 8 INCH AREA, FORWARD ENTRANCE FLOOR SUPPORT. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)SDR USAA050325Skin · puncturedPIT - FOUND SKIN PUNCTURED .5 INCH BY .5 INCH, BS 727A PLUS 10 AT BL 0. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 79988. (M)SDR USAA050353Skin · chafedPIT - Q4 - SLAT, 8 INCH LONG X 3 INCH WIDE AREA, CHAFED. NR 4 SLAT IB T/E LOWER SKIN SURFACE. INSTALLED FILLER AND INTERNAL DOUBLER, KEY CORE AND TOP DOUBLER, SEALED EDGE AND REFINISHED IAW SRM. (K)SDR USAA050335Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 8 INCHES, STATION 312. CORROSION LEVEL 1, TASK C53-107-01. REMOVED AND REPLACED PER SRM AND IPC 53-4200 FIG 2. (M)SDR USAA050328Channel · crackedPIT - FOUND CARGO FLOOR CHANNEL AND SUPPORT ANGLE WITH CRACKS, APPROX .5 INCH CRACKS, FS 500G, RBBL 6. MANUFACTURED AND INSTALLED CARGO FLOOR CHANNEL AND SUPPORT ATTACH ANGLE PER SRM 53-00-53. (M)SDR USAA050327Support · crackedPIT - FOUND ANTENNA SUPPORT CRACKED 1.5 INCH, 1 INCH, .6250 INCH AT STATION 727D S27L AND S27R. FABRICATED REPAIR ANGLE, TRIMMED, FITTED, HEAT TREATED PER SRM 53-60-01. (M)
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