JASC 5100

Service difficulty reports · 4,244

Reports filed under 5100 · Standard Practices/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 = '5100'
  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.

SDR DL76L070783Unknown · unknownRT ENG VALVE AND SPAR VALVE FAIL TO OPEN DURING START. RESET SPAR VALVE C/B, VISUAL INSP SPAR VALVE OK. RESET FIRE HANDLE ENG RUN TEST GOOD.Jun 22, 2007 · N197DN · Boeing 767332SDR QXEA200701038Unknown · unknownSEA FLIGHT NR 2312: DURING CLIMB, BOTH FA'S REPORTED A 1/4 INCH WIDE BY 2 INCH LONG CRACK IN BOTTOM LEFT REAR OF L2. DURING LANDING FA REPORTED DOOR MOVEMENT AND EXPANSION OF CRACK. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AFT PASSENGER DOOR SEAL WJun 22, 2007 · N414QX · Bombdr DHC8402SDR DLM90070875None · noneTEMP REPAIR INSTALLED ON FUSELAGE SKIN AT RT CANT FRAME STA 1531 APPROX 16 IN UP FROM DOOR CUT OUT. REMOVED TEMP REPAIR AND INSTALLED PERM. REPAIR IAW MD90 SRM 53-00-01 FIG 4 VOL I.Jun 21, 2007 · N906DA · Doug MD900SDR 07FDEA02192Plate · noneOLD REPAIR DOUBLER AT C20, P51-54 RT, NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR PERFORMED BY INSTALLATION OF NEW EXTERNAL DOUBLER IAW EA 6-5313-106478 AND RAS/DABRE/7007753/2007 ISSUE "A".Jun 19, 2007 · N731FD · Airbus A300B4605RSDR DLM88070776None · noneDURING SCHEDULED INSPECTION OF THE OVERWING HEATER BLANKET AN ADDITIONAL VOID WAS REPORTED IN THE BONDLINE BETWEEN THE HEATER BLANKET AND THE WING UPPER SKIN. ENGINEERING EVALUATION DETERMINED THE VOID WAS NOT NEW. THE DIFFERENCE FROM PRIOR INSPECTION WAS BEJun 18, 2007 · N903DE · Doug MD88SDR 2007UALA02107Structure · damagedEXTERIOR DAMAGE DUE TO JETWAY COLLISION.Jun 18, 2007 · N806UA · Airbus A319131SDR 2007UALA02092None · noneFLIGHT DIVERTED DUE TO REPORT OF FUMES IN THE CABIN ISOLATED TO THE NR 2 ENGINE. [07-17-07] CHECKED APU INLET & FOUND INTAKE SCREEN FULL OF CICADAS. SUSPECT ALL SMOKE AND ODOR RELATED LOG ITEMS CAUSED BY CICADAS WHICH WERE BURNED BY LOAD COMPRESSOR OF APUJun 18, 2007 · N781UA · Boeing 777222SDR DL764070735None · noneAFTER PUSHBACK CABIN STARTED TO DESCEND AT 2000FM AND BOTH AUTO CONTROLLERS FAILED, RETURNED TO GATE. BITE CK BOTH CONTROLLERS ALL CKS NML. RESET, TESTS NORMAL FOR SVC.Jun 17, 2007 · N835MH · Boeing 767432ERSDR TRAX200700879None · nonePAX DOOR INNER SKIN CRACKED UNDER STEP 832ET (FWD SIDE). [06-28-07] UPON FURTHER EVALUATION FOUND TO BE LIMITED TO PAINT ONLY.Jun 15, 2007 · N886AS · Cndair CL6002B19SDR COMA0760434None · noneTEMPORARY REPAIR INCORPORATED FOR LEFT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE LEFT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.Jun 13, 2007 · N960CA · Cndair CL6002B19SDR COMA0760433None · noneTEMPORARY REPAIR INCORPORATED FOR RIGHT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE RIGHT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.Jun 13, 2007 · N960CA · Cndair CL6002B19SDR DHL2007803542None · noneREMOVE REPAIR BELOW CARGO DOOR AT STA 176 AND INSPECT AREA. INSTALL A NEW REPAIR IAW SRM (PERMANENT) OR APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-53-11 REV IR DATED 06-01-0Jun 10, 2007 · N803DH · Doug DC873SDR DHL2007803536None · noneREMOVE REPAIR BELOW MAIN CARGO DOOR AT STA 226 AND INSPECT AREA. INSTALL NEW REPAIR IAW SRM (PERMANENT) AND APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-08-07, DWG NR AD42-53-112 REV IR DATED 06-Jun 10, 2007 · N803DH · Doug DC873SDR DHL2007803533None · noneRT INBD VANE SLOT HAS AN INTERIM REPAIR AT STA XILD 42 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-2007, DWG NR AD42-57-107 REV IR DATED 05-21-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIOJun 8, 2007 · N803DH · Doug DC873SDR CA070607006Hose · leaking(CAN) HOSE PN-AE366372460330 REPLACED DUE TO SHEDULED MAINTENANCE AND LEAK CHECKED SERVICEABLE, AFTER 1.4 HRS AND 4 CYCLES FOUND LEAKING DURING GROUND HANDLING. HOSE REPLACED AND LEAK CHECKED SERVICEABLE (TC NR 20070607006)Jun 6, 2007 · Cessna 208BSDR VNAA0706005None · noneCLT - FLT 2292 - CREW REPORTED ON TAKEOFF SEVERAL BIRDS STRUCK THE AIRCRAFT ON THE RIGHT WING, THE NOSE WHEEL ASSEMBLY AND ALSO THE RIGHT ENGINE. CREW CONTINUED ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT WING FOR DAMAGE AND FOUND Jun 6, 2007 · N708PS · Cndair CL6002C10SDR DHL2007803544None · nonePERFORM MODIFICATION REPAIR TO THE L2 DOOR, FWD, LOWER CORNER IAW AD2000-20-08, S/B 53-075 AND SR08530021. MAKE ENTRY IN AIRCRAFT LOGBOOK AND PERMANENT RECORD (337 FORM) MAJOR REPAIR (AMOC). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-22-07, BOEING MJun 5, 2007 · N803DH · Doug DC873SDR UH02007F00000None · noneDURING PRACTICE AUTOROTATION, ENGINE SHUTDOWN DUE TO THROTTLE INADVERTENTLY CLOSING INTO FUEL CUTOFF POSITION. STUDENT`S LEG CONTACTED IDLE, IDLE RELEASE BUTTON ON COLLECTIVE STICK HEAD AND THIS ALLOWED THROTTLE TO ROTATE BEYOND IDLE POSITION. HAVE CONTACTEDJun 1, 2007 · N411HU · Scwzer 269DSDR QXEA200700870Unknown · unknownSEA FLIGHT NR 2496: CHECK PFD 1 ILLUMINATED. 3 SECONDS LATER, CHECK ED ILLUMINATED. RAN PFD 1 CHECKLIST. CAUTION DID NOT GO AWAY. RAN SECOND CHECKLIST, ED MESSAGE WENT AWAY. MAINTENANCE REINITIALIZED PFD'S AND ED. ALL FAULTS WENT AWAY AND DID NOT REAPPEAJun 1, 2007 · N405QX · Bombdr DHC8402SDR QXEA200700936None · noneC1 OKC - COMPLIED WITH NR 2 DAMAGE NR 1. REPAIRED IAW SRM 51-42-10, 51-12-00, 51-42-06.May 31, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700935None · noneC1 OKC - COMPLIED WITH NR 3 DAMAGE NR 4. REPAIRED IAW REO670-53-00-123.May 31, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700934None · noneC1 OKC - COMPLIED WITH NR 4 DAMAGE NR 5. REPAIRED IAW REO670-53-00-123.May 31, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700933None · noneC1 OKC - COMPLIED WITH NR 5 DAMAGE NR 6. REPAIRED IAW REO670-53-00-123.May 31, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700932None · noneC1 OKC - COMPLIED WITH NR 6 DAMAGE NR 7. REPAIRED IAW REO670-53-00-123.May 31, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700931None · noneC1 OKC - COMPLIED WITH NR 7 DAMAGE NR 8. REPAIRED IAW REO-53-00-123.May 31, 2007 · N619QX · Cndair CL6002C10SDR 2007UALA01749Skin · noneUPPER FUSELAGE SKIN UNDER DORSAL FIN LT SIDE HAS WORN AREAS FROM BS 908 TO 927. [06-26-07] MAJOR REPAIR: ACCOMPLISHED A FPI INSPECTION NO DEFECTS FOUND AREA TREATED AND PRIMED AND INSTALLED WEAR STRAPS PER AAR EA REV IR EAI070361.May 31, 2007 · N365UA · Boeing 737322SDR QXEA200700929None · noneC1 OKC - REFERENCE ITEM 2 DAMAGE NR 1 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107.May 27, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700928Unknown · unknownC1 OKC - REFERENCE ITEM 4 AND 6 DAMAGE NR 2A AND 2B PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107.May 27, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700925None · noneC1 OKC - REFERENCE ITEM 10 DAMAGE NR 4 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107.May 27, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700927Unknown · unknownC1 OKC - REFERENCE ITEM 8 DAMAGE NR 3 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107.May 25, 2007 · N619QX · Cndair CL6002C10SDR QXEA200700926Unknown · unknownC1 OKC - REFERENCE ITEM 12 DAMAGE NR 5 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107.May 25, 2007 · N619QX · Cndair CL6002C10SDR C2XA07IA122Coupling · looseIAH - FLIGHT 2479, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AND FWD CABIN ON LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 PACK ON MEL 21-60-05/1 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHTMay 23, 2007 · N28529 · Emb EMB135LRSDR 07FDEA01904None · nonePREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF INBOARD FLAP WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEZ EA 6-5750-8181May 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01898None · nonePREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 67-139 RIB2-3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-818May 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01896None · nonePREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 3 WS 1246-1311 RIB 20-21. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-40-00 FIG 102May 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01895None · nonePREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS270-339 RIB 5-6. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IN ACCORDANCE WITH SRM 57-40-00May 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01894None · nonePREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IAW SRM 57-40-00. REPAIR IS CMay 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01891None · nonePREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, SPOILER 2 WS 270-339 RIB5-6. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. A VISUAL INSPECTION AND A TAP TEST WERE PERFORMED IN ACCMay 21, 2007 · N452FE · Airbus A310222SDR 07FDEA01880None · nonePREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS207-270 RIB4-5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-8181May 21, 2007 · N452FE · Airbus A310322SDR 07FDEA01879None · nonePREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS0-139 RIB1-3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81810.May 21, 2007 · N452FE · Airbus A310222SDR 2007FA0000401Housing · crackedCRACK IN PART ID.May 21, 2007SDR 07FDEA02202Flap · misrepairedPREVIOUS REPAIR FOUND LOCATED ON THE RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 0 TO WS 67. REPAIR REQUIRES MAJOR/MINOR EVALUATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAMay 14, 2007 · N452FE · Airbus A310222SDR FDKA200700260None · noneASH 2864 PHX - FWD FA LIFEVEST INSPECTION EXPIRED. MX INSPECTED THE LIFEVEST AND APPLIED A NEW INSPECTION LABEL.May 11, 2007 · N17275 · Cndair CL6002B19SDR VNAA0705001Unknown · unknownCREW REPORTED THE PLANE SUDDENLY JUMPED ON TAKEOFF ROLL AT 20-30 KTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MAIN LANDING GEAR AND FOUND NO DEFECTS. MAINTENANCE ALSO PERFORMED A TAXI CHECK May 10, 2007 · N254PS · Cndair CL6002B19SDR MASA200700250None · noneASH 7220 ROC - PORTABLE O2 BOTTLE USED FOR MEDICAL EMERGENCY. CONTRACT MX SERVICED AND CLEANED THE MASK ON THE PORTABLE O2 BOTTLE.May 8, 2007 · N571ML · Cndair CL6002B19SDR 2007FA0000585Bolt · brokenTHE BOLTS FAILED DUE TO LANDING WITH WHEEL LOCKED. THINK THE BOLTS WERE FINE BEFORE THIS INCIDENT. (K)May 7, 2007 · N5149 · Scwzer G164ASDR MASA200700242None · noneASH 2843 PHX - EMERG EXIT LIGHTS AT PAX AND SERVICE DOORS INOP. NO DEFFECT NOTED, LIGHT WAS GLOW TYPE.May 3, 2007 · N7264V · Cndair CL6002B19SDR MASA200700223None · noneASH 7463 ROC - FWD CABIN PBE VSI WAS PROTRUDING AND PACKAGE FELT SPONGY. MX FOUND GOOD TO FLY FOR 36 HOURS AND AIRCRAFT WAS RELEASED FOR SERVICE.Apr 23, 2007 · N592ML · Cndair CL6002B19SDR 2007FA0000367Doubler · fatiguedTHE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER FATIGUE CRACKING ON BOTH. THE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN. CURRENTLY THE PAApr 20, 2007 · Cessna 650SDR 2007UALA01144Unknown · vibrationDURING CLIMB-OUT, AIRCRAFT VIBRATION VARYING SPEEDS AND ALTITUDES. CRUISE SMOOTH. [SUP 06-06-07] REPLACED ALL THREE RUDDER ACTUATOR ROD ENDS.Apr 13, 2007 · N428UA · Airbus A320232
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