JASC 5101
Service difficulty reports · 482
Reports filed under 5101 · Aircraft Structures, 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 jasc_code = '5101' 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 jasc_code = '5101' 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 07FDEA02201None · nonePREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO AN SDR DXTA200702171Unknown · unknownAT FL190 AND 190KIAS, A SUDDEN LOUD, LOW 'THUD' WAS HEARD AND FELT. 3 SECONDS LATER IT WAS HEARD AGAIN. PASSENGER THOUGHT IT CAME FROM BENEATH HIM AT CABIN SEAT POSITION 5/6. NOISE/THUD WAS FELT AND HEARD THROUGH ENTIRE AIRFRAME. PERFORMED VISUAL INSPECTIOSDR SIMA200712003Unknown · vibrationVIBRATION FELT INFLIGHT BETWEEN ROW 3 AND ROW 7.SDR RAIA00703066Unknown · unknownFLT NR 7901 - ROA - FLIGHT ATTENDANT & PASSENGER REPORTED LARGE STREAM OF VAPOR FROM UNDER WING DURING CLIMBOUT. TANK 2 INDICATION SHOWED GREATER LOSS OF FUEL THAN THE LEFT TANK. MAINTENANCE FUELED AIRCRAFT WITH 11290 LBS AND INSPECTED NO LEAKS NOTED.SDR 07FDEA00329Unknown · unknownOLD REPAIR ON TOP CAP BEAM AT C62 LT. REPAIR WAS RENEWED IAW SRM 53-10-15, FIG 207.SDR COMA0760108Unknown · unknownFLIGHT 5270 - ANTI-ICE DUCT MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF WING ANTI-ICE SYSTEM, NO DEFECTS NOTED. OPS CHECK GOOD.SDR 2007UALA00217Unknown · vibrationMODERATE TO SEVERE VIBRATIONS FELT IN AFT CABIN & FLT DECK FLOOR ON CLIMBOUT. VIBRATIONS SUBSIDED AT LEVEL OFF. CONDITIONS REAPPEARED ON SUBSEQUENT FLIGHT. ACCOMPLISHED ELEVATOR INTEGRITY CHECKS. ALL 4 SERVOS REQUIRED ADJUSTMENT TO .5 DEGREES NOSE UP. FRSDR CHQA200700004Unknown · vibrationFLIGHT 3257 - IAH-MSP - WHILE CLIMBING THROUGH 3,000 FEET, RECEIVED MULTIPLE "STALL FAIL" MESSAGE ON THE EICAS. THROUGH 3,500 FEET, HEARD A NOISE IN THE FRONT OF THE AIRCRAFT. THE NOISE BECAME LOUDER. LEVELED OFF AT 4,000 FEET AND NOTIFIED ATC AND BEGAN TO SDR 2007UALA00201Unknown · vibrationA/C VIBRATION FELT ON CLIMB-OUT 3 TIMES. CHECKED ELEVATOR FOR FREE PLAY, RIGHT SIDE HAD ENOUGH PLAY TO WARRANT REPLACEMENT OF YELLOW SERVO CONTROL. AFTER REPLACEMENT OF SERVO CONTROL PLAY WAS WITHIN STANDARDS. OPS CHECKED GOOD. ACCOMPLISHED INSTALLATION INSDR TRAX200600661Beam · crackedSUSPECT CENTER BOXBEAM CRACKED BELOW UPPER FIRELOOP CLIP. JOB COMPLETE RII COMPLETED IWA E0 600-53-0072BSATIFACTORY REPAIR OF ENGINE BOX BEAM, UPPER AND LOWER ANGLES 8/31/2006// MB14369 EC EO 600-53-72 0001 COMPLIED WITH. PER REO 601R-53-61-345. (SUPPLEMENTALSDR TRAX200600607Engine · bird ingestionBELIEVE TO HAVE IMPACTED SOMETHING IN FLIGHT SHORTLY AFTER TAKEOFF. IMPACT SOUNDED LIKE IT CAME FROM LEFT SIDE OF A/C. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. A/C RETURNED TO ATL AFTER T/O INSPECTED A/C FOUND BIRD REMENENTS UNDER LT. WING , CLEANED AND SDR ASMF200607015Rivet · looseREPORTED A WATER LEAK IN THE OVERHEAD PANEL NEAR TO THE CABIN CREW DOOR. AIRCRAFT WAS SENT TO THE HANGAR AND INTERIORS AND AIR CONDITIONING DUCTS WERE REMOVED, DETECTING 30 RIVETS LOOSEN BETWEEN LONGERONS 1 TO 4, FROM STATION 148 TO 180; IT PROMOTED A PRESSURISDR AWXA200601365Structure · corrodedFOUND CORROSION ON R2 INNER STRUCTURE BS 954-993 RBL 43-52 WL 208. MAINTENANCE REMOVED AND REPLACED R2 INNER STRUCTURE BS 912-1006 RBL 43 WL 208 IAW B737-300 SRM 51-40-02-0G PARA 4B AND 7D, FIGS 3, 4, 8, 12.SDR ASMF200607014Door · ground damageAIRCRAFT WAS HIT BY TELESCOPIC CORRIDOR ON THE PASSENGERS DOOR. PASSENGER DOOR WAS INSPECTED AND COVER DOOR WAS REMOVED FOR REWORK. LOWER SUPPORT OF LEFT FORWARD DOOR WAS STRAIGHTENED FROM COVER INSIDE IAW DOCUMENT PRODUCT STANDARD BAC5300.SDR ASMF200607013Structure · ground damageDURING OVERNIGHT CHECK, AIRCRAFT WAS HIT BY A CARGO CONTAINER, BETWEEN LT LONGERONS 25 AND 26 PRODUCING A DENT OF 5 INCHES OF DIAMETER AND CRACK IN THE CENTER OF 2 INCHES BETWEEN STATIONS 303 AND 312. PENDING FINAL WORKS.SDR VNAA0607022Structure · bird strikeCREW REPORTED A BIRD STRIKE TO THE TAIL ON TAKEOFF. MAINTENANCE CLEANED AND INSPECTED THE AREA. NO DAMAGE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR 2006UALA01355Structure · vibrationFLIGHT REPORTED A VIBRATION ON CLIMBOUT IN THE COCKPIT & A STRONGER VIBRATION IN THE TAIL & AFT GALLEY. ACCOMPLISHED AMM5-50-00. VIBRATION DECICION TREE SUGGESTS TYPE 1 ELEVATOR AS MOST PROBABLE CAUSE. MAINTENACE TIP 53-005 ALSO ACCOMPLISHED. AM27-34-00-20SDR VNAA0606016Paint · damagedCREW REPORTED LIGHTNING STRIKE. EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS WERE PERFORMED. PAINT DAMAGE NOTED AND REPAIRED ON NOSE, RADOME AND VHF 2 ANTENNA. THE AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.SDR 2006UALA01261Skin · damagedDENTS AT STA 1660 BETWEEN STR 43R & STR 44R AND BETWEEN STR 44R & STR 45R. BOTH DENTS ARE APPROX 7 INCHES IN DIAMETER, SMOOTH BUT WITH A .25 INCH DEPTH. FWD OF AFT PIT BELOW FLOOR LEVEL. DENT AT STA1660 BETWEEN STR 43R & STR 44R, DENT AT STA 1660 BETWEEN STR4SDR VNAA0605004Structure · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DURING CRUISE. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE LT HORIZONTAL STAB TIP AND SEVERAL SPOTS ON THE RT FUSELSDR GUUA95253042606ASpar · crackedDURING SCHEDULED ROUTINE MX DISCOVERED 2.0 INCH CRACK IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REPAIR.SDR 06FDEA1485Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1166 STR 30 IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR UIEA200600064Repair · unknownFOUND FUSELAGE SKIN, SECTION 46 NON-STANDARD REPAIR INSTALLED AT AFT UPPER EDGE OF MED 4R CUT OUT, BETWEEN STR 17R & 19R. C/OUT HFEC ON TRIM LINE AND EXISTING FASTENER HOLES WITH DOUBLER REMOVED, NIL FINDING. C/OUT HFEC ON FUSELAGE SKIN WITH DOUBLER AREA, NISDR 06FDEA1242Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: LT WING, LEADING EDGE, LOWER SIDE, XORS 506: EXISTING REPAIR. NO ACTION REQUIRED. REPAIR MEETS SRM 57-10-00 FIG 68 REQUIREMENTS.SDR 06FDEA1182Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON FWD PIT CROSSBEAM AT FR 25 TO FR 25, FS 1711 TO FS 1711 AND Y72 TO Y72. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APSDR 06FDEA1166Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND STA 888-905, STR 42-43, RT, FWD CARGO DOOR, LWR FWD ANGLE: EXTERNAL REPAIR DOUBLER. NO ACTION TAKEN, REPAIR MEETS CRITERIA OF SRM 52-10-00 FIG 17.SDR 06FDEA1165Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 555-575, STR 46-48, LT, EXTERNAL REPAIR DOUBLER. RECOMMENDED ACTION: NO ACTION REQUIRED, REPAIR MEETS SRM 53-20-00 FIG 2 CRITERIA.SDR 06FDEA1126Repair · noneHORIZONTAL STAB O/B SECTION LOWER SIDE HAS EXISTING REPAIR XCH 44.5567. REMOVED PAINT IAW SRM 51-21-01 PAR 21 VOL 2, PERFORMED NDI IAW NDT SP 4-6 FOUND STUD PANEL IS IN 7075-T651 COLD MATERIAL, TREATED AREA IAW SRM 51-21-01VOL 2. PERFORMED INSPECTION ON REPASDR 06FDEA1139Repair · noneFOUND MAIN CARGO COMPT STA 791-830 X-8.5 EXISTING SEAT TRACK SPLICE REPAIR. PERFORMED VISUAL INSPECTION OF SEAT TRACK SPLICE REPAIR FOR CRITERIA REQUEST BY EO NR 8-5100-7-5001P2. FOUND REPAIR IN COMPLIANCE.SDR 06FDEA1102Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 65 TO FR 65, FS 3514 TO FS 3514 AND Y 20. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION ASDR 06FDEA1100Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 37 TO FR 37, FS 2029 TO FS 2029 AND YE 57 TO YD 81. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICASDR 06FDEA1095Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1128 AND YD 95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION ASDR 06FDEA1093Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON LEFT HAND MCD SEAT TRACK AT FR 54.3 TO FR 55/58, FS 3090 TO FS 3143, AT - YD95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATSDR 06FDEA1089Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 475-505 STR 30-32 LT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, THE REPAIR IS ALREADY APPROVED BY A.A. ES 07349.SDR 06FDEA1088Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 275-304 STR 28-29 LT, 2 FLUSH PATCH WITH INTERNAL DOUBLER. NO ACTION REQUIRED. REPAIR IS CONFORM TO SRM 53-20-00 FIG 11.SDR 06FDEA1084Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MDC FLOORBEAM AT FR 12A/13, FS 1091/1125, AT YD953. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED RESDR 06FDEA1077Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND SIDE NUMBER THREE SLAT OUTBOARD END, WS 1868 TO WS 1868. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVSDR 06FDEA1076Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND SIDE OF LOWER WING SURFACE INBOARD OF WING TIP, RIB 31, WS 1868. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION ANSDR 06FDEA1075Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON R2 DOOR AT FR 74 TO FR 74, FS 3998 TO FS 4024, STR 26 TO STR 27. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED SDR 06FDEA1073Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE CROWN RIGHT HAND SIDE AT FR 10 TO FR 10, FS 962 TO FS 982. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVSDR 06FDEA1072Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 87 TO FR 87, FS 4625 TO FS 4645, STR 8 TO STR 8. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATIONSDR 06FDEA1071Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 64 TO FR 64, FS 3451 TO FS 3471, STR 7 TO STR 8 AND AFT AND BELOW UPPER AFT ANTENNA. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUSDR 06FDEA1070Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 75A TO FR 75A, FS 4095 TO FS 4095, STR 23 TO STR 24, AND AFT OF R2 DOOR CUTOUT LOWER FAIL SAFE RING. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPSDR 06FDEA1069Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 73A TO FR 73A, FS 3964 TO FS 3964, STR 23 TO STR 24, AND FWD OF R2 DOOR CUTOUT LOWER FAIL SAFE RING. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPSDR 06FDEA1068Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 80/82 TO FR 83, FS 4370 TO FS 4430, STR 32 TO STR 34. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICSDR 06FDEA1067Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 77 TO FR 77, FS 4181 TO FS 4181, STR 28 TO STR 29. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATISDR 06FDEA1066Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 73 TO FR 74, FS 3938 TO FS 3998, STR 29 TO STR 31 AND BELOW L2 DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/SDR 06FDEA1065Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 39 TO FR 39, FS 2227 TO FS 2265, STR 35 TO STR 35. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATISDR 06FDEA1064Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 12A TO FR 12A, FS 1081 TO FS 1101, AND LOCATED ABOVE TOILET SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR SDR 06FDEA1063Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 12 TO FR 12A, FS 1067 TO FS 1091, AND LOCATED ON TOILET SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJO
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