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.
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
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 06FDEA04161Skin · unknownFOUND EXTERNAL REPAIR AT APPROX STA 1343 RT SIDE NR 2 NACELLE SKIN (STR 9R-S10R). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACOMPLISHED USING FAA APPROVED DATA. REPAIRED AREA WITH A SINGLE DOUBLER TYPE REPAIR REF SRM 51-40-2 SDR 06FDEA04158Unknown · contaminatedLANDED ON ORD RW09R WITH CONTAMINATED RW. STOPPED WITH LEFT MAIN GEAR OFF THE LEFT SIDE OF THE RW. RT GEAR STILL ON THE RW. NOSE SLIGHTLY OFF THE LEFT. PSC COMPLIED INSPECTION IAW AMM 05-51-24-0. AIRCRAFT FOUND TO BE AIRWORTHY.SDR 2006UALA02313Unknown · vibrationCREW REPORTED A SEVERE VIBRATION FROM TOUCHDOWN THROUGH ROLLOUT. FOUND NLG TORSION LINKS WORN BEYOND IN-SERVICE LIMITS. REPLACED LOWER NLG TORSION LINK ASSY.SDR QXEA200603375Skin · damagedC4 PDX - TEMPORARY REPAIR FOR LIGHTNING STRIKE AT STATION X167.00 BETWEEN STRINGERS 30 AND 31 CHERRY FASTENER INSTALLED IAW RD 8-53-65013 REQUIRES PERMANENT REPAIR. REPAIRED IAW RD 8-53-6798.SDR 2007FA0000021Pin · mismanufacturedTWO OCCURRENCES OF A RETAINING PIN HOLDING THE UNIVERSAL-JOINT TOGETHER, HAVING INSUFFICIENT PEENING TO RETAIN THE PIN, HAS BEEN IDENTIFIED IN BUILD OF THE UNIT BY THE ACTUATOR/DRIVE SHAFT MFG. THE PIN IS THEREFORE NOT SUFFICIENTLY RETAINED AND MAY WALK OUT OSDR 06FDEA04057Unknown · unknownDURING U/S INSPECTION ON CONSTANT AND OUTER SEC STB, FOUND CRACKS WHEN SHOWN AN ATTACHED SHEET. REMOVED PANEL ALC7206-1 IAW SB 55-16 GROUP 1, CLEANED BOLTS AND INSPECTED IAW SB 55-16 PAGE 28 STEP K. PANEL INSTALLED NEW P/N ALC7206-1 IAW SB 55-16 GROUP 1 ANDSDR IXXA06SMN416SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR AT STATION XS430.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMSDR IXXA06SMN415SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR AT STATION XOLDI6.224. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE RESDR IXXA06SMN337SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, EXISTING REPAIR AT STA FS 1500, LONGERON 16 RIGHT HAS AN INTERIM REPAIR. REMOVED EXISTING REPAIR DC8 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND DAMAGE REMOVED. FABRICATED NEW REPAIR DOUBLESDR DL76G060910Unknown · unknownAFTER TAXI OUT, ATC HOLD, ENGINES SHUTDOWN WITH APU. ON RE-START OF BOTH ENGINES CABIN ALT AUTO 1 AND AUTO 2 ILLUMINATED. AUTO PRESSURIZATION INOP. ACCOMPLISHED FIM 21-31-00 FIG 103 AND 109. OPS CHECK OK.SDR 2006FA0001056Pin · brokenLOCKDOWN PINS BROKE AT GROOVE FOR ROLL PINS. THIS ALLOWED THE PINS TO MOVE OUT OF ACTUATOR BEARING END AND JAM THE ACTUATOR. IN THE UNLOCKED POSITION, SEB95-20 ACTUATOR DOWNLOCK PIN. INSPECTION SAYS TO CHECK FOR LOOSE PINS. THESE PINS WERE NOT LOOSE IN THESDR SIMA200628201Unknown · unknownORD - FLT 3900 - DURING CLIMB-OUT A SHARP THUMP WAS FELT IN THE FORWARD PORTION OF AIRCRAFT AND SOUNDED LIKE SOMETHING HAD CONTACTED THE AIRCRAFT. ALTITUDE WAS 23,000 FEET AND AIRSPEED 250-260 KNOTS, SOUND AND THUMP WAS FELT AND/OR HEARD AT LEAST TO ROW 6 IN SDR 06FDEA03492None · noneEXISTING REPAIR (DOUBLER), NR 2 AIRCON ACCESS DOOR AT MOST UPPER EDGE (SKIN P/N ACA3822-7). NEW SKIN ON DOOR FRAME INSTALLED AS PER SRM 51-35-01 VOL2.SDR 06FDEA03489None · noneFOUND EXISTING REPAIR, CENTER CARGO DOOR JAMB FWD EDGE STA 1780 (SKIN ASSY P/N AFA7158-503) (ER/A271080-14). NEW REPAIR DOUBLERS AND FILLER INSTALLED AS PER SRM 51-33-01 VOL2 (MAJOR REPAIR).SDR 06FDEA03488None · noneFOUND EXISTING REPAIR, CENTER CARGO DOOR JAMB AFT EDGE STA 1780 LONGERON 40R (SKIN ASSY P/N NGA6313-515) (ER/A361240-14). NEW REPAIR DOUBLERS AND FILLER INSTALLED AS PER SRM 51-33-01 VOL2 (MAJOR REPAIR).SDR NSVA200600156Unknown · unknownRIGHT PROP AUTOFEATHERED INFLIGHT, DURING APPROACH TO LANDING UPON MOVING PROPS FULL FORWARD. CLEANED AND INSPECTED ALL RT ENGINE NOSE SECTION CONNECTOR PLUGS, NO DEFECTS NOTED AT THIS TIME. CLEANED AND INSPECTED ALL RT ENGINE NOSE SECTION WIRING HARNESS FORSDR SIMA200626801Unknown · smokeTOWER REPORTED WHITE VAPOR COMING FROM AIRCRAFT ON CLIMBOUT FROM DFW, RETURN TO DFW. (M)SDR 2006FA0001010Rod End · brokenROD END BROKE AT POINT OF ATTACHMENT ON SERVO ARM. APPEARS BOLT MAY HAVE BEEN OVER TORQUED AT SOME POINT WHICH CAUSED A STRESS CRACK AND FAILURE OF BOLT AT POINT OF ATTACHMENT. TORQUE BOLT AT TIME OF INSTALLATION. (K)SDR CHQA200600121Tape · dislodgedFLIGHT 7846 - YYZ-IAD - AT FL260, FLIGHT CREW NOTICED A -POPPING- SOUND FROM F/O'S WINDOW AND -HISSING- SOUND. EICAS INDICATED QUICKLY RISING CABIN ALTITUDE. BOTH CREW MEMBERS DONNED OXYGEN MASKS AND EXECUTED CABIN DEPRESSURIZATION AND EMERGENCY DESCENT MEMOSDR 06FDEA03261Pressure Panel · unknownHORIZONTAL PRESSURE PANEL BETWEEN STA 535 AND 555 X= 86 LT SIDE WEB FOUND EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5330-99720. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016410/N01410 AND IAW EA NR 8-5330-99720.SDR 06FDEA03242Unknown · unknownEXISTING EXTERNAL DOUBLER REPAIR APPROX 11" BY 5" AT STA 440, RT STRINGER 27. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER AT STA 440 STR 27R AND REPLACED IAW SRM SDR SB06088Unknown · unknownDURING CRUISE, EN ROUTE FROM CLT TO ROC, CREW REPORTED THE NR 2 ENGINE FLAMED OUT (AND THE CROSSFEED LIGHT EXTINGUISHED) WHILE CROSSFEEDING FUEL AT FL370. CREW DECLARED AN EMERGENCY TO CLEAR TRAFFIC AND DESCEND TO LOWER ALTITUDE AND WAS ABLE TO RESTART NR 2 ESDR 2006UALA01703Unknown · unknownCREW REPORTS ALTERNATE LAW DISPLAYED WITH NO FLIGHT CONTROL FAULTS. REPLACED NR 2 ELAC AND ACCOMPLISHED TEST, TEST NORMAL.SDR 2006UALA01689Skin · ground damageAIRCRAFT STRUCK BY JETWAY. REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 06FDEA03056Skin · misrepairedDURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 294 AT STR 21R. REMOVED AND REPLACED REPAIR REF: SRM 53-30-3 WO NR 33554, SNRM NR N00420. REMOVED EXT REPAIR ASDR 06FDEA3035None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT AFT COMP´T DOOR FRAME BETWEEN FS 63/64 AND STRINGER BETWEEN 40/44 RT. REPAIR REQUIRES EVALUATION SDR 06FDEA3036None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 64/67 AND BETWEEN STRG 33/40 RT . REPAIR REQUIRES EVALUATION FORSDR 06FDEA3037None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 66/68 AND BETWEEN STRG 48/54 RT . REPAIR REQUIRES EVALUATION FORSDR 06FDEA3038None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT FS4715/4760, FS 89/90, STRG 33/38 NEXT TO APU INLET. REPAIR REQUIRED EVALUATION FOR MAJOR/ MINOR DSDR 06FDEA3039None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIONSDR 06FDEA3040None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATIONSDR 06FDEA3041None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT. FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FS 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THESDR 06FDEA3042None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND REPASDR 06FDEA3043None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION ASDR 06FDEA3044None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIOSDR 06FDEA3045None · noneFOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3054None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVESDR 06FDEA3053None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTB LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3052None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3051None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3050None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3049None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3048None · noneFOUND REPAIR LOCATED LT INBD FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3047None · noneFOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INBD OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA3046None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA03004Skin · misrepairedDURING C-1 CHECK AGING AIRCRAFT INSPECTION, IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA.640 BETWEEN STRINGERS 24L AND STR 28L. REMOVED AND REPLACED REPAIR PER B727 SRM 53-30-3 FIG 5 PG 22. INSTALLEDSDR 06FDEA03003Skin · misrepairedDURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 950 AT STR 28L. REMOVED AND REPLACED REPAIR REF: B727 SRM 53-30-3 FIG 1 PG 8 WO NR 33554, SNRM NR N00556. INSTSDR MALA060515Skin · delaminatedDURING 4K CHECK IN BNA, FOUND LT ELEVATOR, P/N 7255201-653, S/N 2045, IS CHAFED ON THE OUTBOARD LEADING EDGE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S51031. REF: EAMS WORK ORDER 214265 TASK 3505.SDR 14540810226AUnknown · unknownDURING TAKEOFF ROLL AIRCRAFT PULLED SHARPLY LT THAN BACK STRAIGHT.SDR 06FDEA2912Skin · unknownN01454 EXISTING EXTERNAL DOUBLER REPAIR APPROX. 9.50 INCHES X 14.50 INCHES AT STA. 494 LT STRINGER NR 19 (DOT NR 16) REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AND INS
Back to JASC 5100