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 06FDEA1109Repair · unknownTHREE REPAIRS LOCATED ON LEFT I/B FLAP UPPER SURFACE T/E REQUIRES EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED DATA REF BN00770. REPAIR IAW EA 6-5750-97510.Mar 15, 2006 · N455FE · Airbus A310222SDR 06FDEA1108Repair · unknownREPAIR LOCATED ON LEFT I/B FLAP LOWER SURFACE T/E REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND APPROVED DATA REF N00771. REPAIR WAS DETERMINED TO BE IAW EA 6-5750-97510.Mar 15, 2006 · N455FE · Airbus A310222SDR 06FDEA1082Repair · unknownCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR INSTALLED ON RIGHT OUTBOARD FLAP RIB 15 TO RIB 15, WS 925 TO WS 935. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1078Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT INBOARD FLAP LOWER TRAILING EDGE WEDGE, WS 163 TO WS 189. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED & EVALUATEDMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1085Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND NUMBER TWO SPOILER UPPER OUTBOARD END AT WS 339 TO WS 359. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED AMar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1083Repair · unknownPREVIOUS REPAIR INSTALLED ON LT OUTBOARD FLAP LOWER SURFACE BETWEEN FLAP RIB 4 AND 5 AT WS 1010 TO WS 1030. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. Mar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1081Repair · nonePREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 145 TO WS 177. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGMar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1080Repair · unknownPREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 40 TO WS 86. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE Mar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1079Repair · unknownPREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP LOWER TRAILING EDGE WEDGE, WS 140 TO WS 185. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGMar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1074Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE CROWN LEFT HAND SIDE AT FR 40/41 TO FR 40/41, FS 2294 TO FS 2294, STR 2 TO STR 3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPMar 14, 2006 · N426FE · Airbus A310SDR 06FDEA1047Repair · noneN01048 LOWER FWD CARGO COMP. FLOOR FRAME REPAIR FUSELAGE STA. 560 LBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ** SD ** COMING REPAIRED FRAME PWR SRM 51-40-3.Mar 14, 2006 · N492FE · Boeing 727200SDR 06FDEA1056Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 20 TO FR 20, FS 1446 TO FS 1446, STR 36 TO STR 40, AND FWD LOWER SIDE OF FWD CARGO DOOR CUTOUT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINORMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1045Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1781 STR 39-41 RIGHT, EXTERNAL REPAIR DOUBLER. EXISTING REPAIR WILL BE MODIFIED DURING P TO F CONVERSION (NC 30008).Mar 14, 2006 · N568FE · Doug DC1010SDR 06FDEA1044Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1711 STR 40-42 RIGHT, EXTERNAL REPAIR DOUBLER. REPAIR MEETS SRM 53-50-00 FIG 9 CRITERIA, EXISTING REPAIR REMOVED TO ACCOMPLISH NRC N00307.Mar 14, 2006 · N568FE · Doug DC1010SDR 06FDEA1043Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: BETWEEN STA 979-999 STR 36-39, RIGHT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, REPAIR IS CONFORM TO SRM 53-20-00 FIG 6 SH 3.Mar 14, 2006 · N568FE · Doug DC1010SDR COMA0660243Warning Light · illuminatedFLIGHT 5113 - DURING CLIMBOUT OF GRB RECEIVED A DISPLAY COOL CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. CLEANED DISPLAY FILTER.Mar 13, 2006 · N816CA · Cndair CL6002B19SDR 200603131None · noneFLIGHT 7622 ORD PRIOR TO T/O CREW REPORTS HIGH WINDS WITH CHANGING DIRECTIONS AND 1 HOUR TAXI TIME, OCCASIONAL ADVISORY MESSAGE; PROB 2 FAIL MESSAGE WOULD GO AWAY, ATTRIBUTED TO HIGH WINDS. ON CLIMBOUT EICAS MESSAGES STALL PROTECTION FAIL, AOA LIMIT FAIL, WINMar 13, 2006 · N641RW · Emb ERJ170100SDR MALA060155None · noneFUSELAGE SUSTAINED DAMAGE BY CONTACT WITH PASSENGER'S STROLLER. THE AIRCRAFT IS CURRENTLY BEING EVALUATED FOR DAMAGE ASSESSMENT. RAMP AGENT LOST CONTROL OF BABY STROLLER IN HIGH WIND CONDITIONS AND IT HIT THE R/H PROPELLER WHILE ENGINE RUNNING. INSPECTED AIMar 13, 2006 · N421XJ · Saab 340BSDR 06FDEA1021Repair · unknownLEFT MLG W/W 3EA CRACKS ON OLD REPAIR INBOARD BULKHEAD FROM STA 1471 TO STA 1481 Z-60. REMOVED EXISTING REPAIR IAW SRM 51-35-01 PAGE 1 VOL 2. PERFORMED INSP IAW NDI SPM06- 10-02 CONFIRMED SIGNED CRACK ON INSP AREA. ENLARGED CUT OUT TO ENG LOBE CRACK AND INSMar 13, 2006 · N365FE · Doug DC1010SDR 06FDEA1019Repair · unknownMAIN CARGO COMPT STA 700-735 X-47.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH LOCK FASTENER IAW SRM 57-70-00 FIG 1 VOL 1. AFT REWORK THE EXISTING REPAIR ON SEAT TRACK RETURNED IN COMPLIANCE WITH CRITERIA REQUESMar 13, 2006 · N68054 · Doug MD1010FSDR 06FDEA1016Repair · unknownEXT MOD DOUBLER REPAIR JUST AFT OF NR 9 ON REPAIR LOCATION STA 879-889. REMOVED OLD DOUBLER AND PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1. FAB PARTS IAW DETAIL PARTS TRAVELER F167066/N01066 AND IAW SRM 53-20-00 FIG 6 VOL 1.Mar 13, 2006 · N68054 · Doug MD1010FSDR 06FDEA1014Repair · unknownINT FUSELAGE STA 1154 FOUND PANEL REPAIR. REMOVED OLD DOUBLERS IAW SRM 51-35-01 VOL 2. PERFORMED GVI ON AREA, NO CRACK FOUND, PERFORMED NDI INSPECTION, NO DAMAGE FOUND. TREATED AREA IAW SRM 51-21-01 VOL 2 AND INSTALLED NEW -3, -5, -7, DOUBLERS IAW SRM 53-40Mar 13, 2006 · N68054 · Doug MD1010FSDR 06FDEA1013Repair · unknownFOUND NR 6 REPAIR UPPER SKIN RIGHT OUTBOARD FLAP. REMOVED SKIN TRIMMED OUT DAMAGED RIBS, FABRICATED NR 3 INTERNAL ANGLE REPAIR AND FILLER REPAIR IAW SRM 57-00-01 FIG 10 VOL 1, REPAIRED AND REINSTALLED NEW SKIN IAW SRM 57-10-00 FIG 7 VOL 1. FAB PART IAW DETAIMar 13, 2006 · N563FE · Doug DC1010SDR CA060314003Unknown · multiple failWHILE CLIMBING THROUGH 15000 FT, THE FOLLOWING WAS ENCOUNTERED: CABIN EMERGENCY LIGHTS FLASHING. THRUST REVERSER ISOLATION VALVE OPEN ILLUMINATED. NOSE GEAR UNSAFE INDICATION (GEAR RETRACTED). DFDR ILLUMINATED. CARGO OVERHEAT/DETECTION FAULT. APU FAILED TOMar 12, 2006 · Boeing 737*SDR 06FDEA1010Repair · noneEXTERNAL DOUBLER REPAIR LEFT HORIZONTAL STAB UPPER T/E PANEL, APPROX 4 X 4 INCHES. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Mar 12, 2006 · N492FE · Boeing 727200SDR AWXA200600467None · noneDURING FLIGHT CREW REPORTED, FWD CARGO DOOR OPEN ECAM MESSAGE. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PLACED THE FORWARD CARGO DOOR INDICATION ON DEFERRAL. DEFERRAL WAS CLEARED ON 03/12/06, PILOT REPORTED THAT AT PUSHBACK RAMPERSMar 11, 2006 · N644AW · Airbus A320231SDR IXXA06SMN092SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP T/E UPPER PANEL HAS NON STANDARD REPAIR BETWEEN XF 415.000 AND XF 418.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1, 2). REMOVED NON STANDARD REPAIR (EXISTING) IAW DC8 SRM 51-1-21. REMMar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN093SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP L/E UPPER PART HAS NON STANDARD REPAIR WORN 1 INCH, XF 346.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR 57-94 DATE 10-01-02. REMOVED DAMAGED PLATING WITH NON STANDARD REPAIR IAW DC8 SRM 57-1-Mar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN094SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP LWR FWD SKIN NON STANDRAD REPAIR, XF 16.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGMar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN095SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 21.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMMar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN097SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 430.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DMar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN085SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RIGHT WING - CTR L/E LWR EXTERNAL PART NON STANDARD REPAIR XFS 335.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4189 DATE 03-07-06, EO SEMAN 2006154 DATE 03-15-06. REMOVED NON STANDARD Mar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN079SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT HORZ STAB L/E UPPER SURFACE HAS NON - STANDARD REPAIR, STA XFS 47.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4188 DATE 03-08-06, EO SEMAN 2006149 DATE 03-15-06. REMOVED NON STANDARMar 9, 2006 · N602AL · Doug DC873FSDR IXXA06SMN070SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LEFT CUSP EXTRUSION UPPER SURFACE FRAME NON STANDARD REPAIR, STA 1560.000 L-20L. PERFORMED MAJOR REPAIR. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED AREA, FABRICATED NEW FRAME SEGMENT P/N 52645791. FABRICATED (02 EA) ANGMar 9, 2006 · N602AL · Doug DC873FSDR 06FDEA0981Repair · unknownMAIN CABIN STA 879 - 939 X = 47.5 EXISTING SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUIRED ON EO 8-5100-7Mar 8, 2006 · N68054 · Doug DC1010SDR 06FDEA0980Repair · unknownMAIN CARGO COMPT STA 615 - 655 X = 8.5 EXISTING SEAT TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED EXISTING SCREWS WITH HI-LOKS IAW SRM 53-70-00 FIG 1 VOL 1. AFT REWORKED ACTION THE SEAT TRACK SPLICE REPAIR RETURNED IN COMPLIANCE WITH CRITERIA REQUIMar 8, 2006 · N68054 · Doug DC1010SDR 06FDEA0979Repair · unknownMAIN CARGO COMPT STA 615 - 655 X = 27.5 EXISTING TRACK SPLICE REPAIR. REMOVED GANG CHANNEL AND REPLACED SCREWS WITH LOCK FASTENERS IAW SRM 53-70-00 FIG 1 VOL 1, AFT REWORKED ACTION OF SEAT TRACK SPLICE REPAIR, RETURNED IN COMPLIANCE WITH CRITERIA REQUIRED ON Mar 8, 2006 · N68054 · Doug DC1010SDR DHL2006760503None · noneACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT HAND HORIZONTAL STABILIZER L/E SKIN AT L/E STA 30.0. INSTALLATION PERFORMED IAW 727 SRM 55-10-3 FIG 2. VERIFIED MATERIAL USED IS 7075-T6 0.063 THIS REPAIR IS CATEGORY A.Mar 7, 2006 · N760AT · Boeing 7272B7SDR DHL2006760501Repair · noneACCOMPLISH IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT WING FIXED LEADING EDGE SKIN AT WS 207.0. ACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT WING FIXED LEADING EDGE SKIN AT WS 207.0. INSTALLATION PERFORMED IAW B-727 SRM 57-30-4 FIG 2. Mar 7, 2006 · N760AT · Boeing 7272B7SDR 06FDEA0977Repair · unknownEXISTING REPAIR STA 720-745 STR 21L-22L IS IAW EXISTING FAA DATA. REPLACE EXISTING REPAIR PER SRM. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FROM 2024- T3 .063 BATCH 1022264 IAW SRM 53-30-3 FIG 2, 4 & 51-30-2, TREATED, PRIMED AND PAINTED IAW SRM 51-10Mar 7, 2006 · N275FE · Boeing 727200SDR 06FDEA0972Repair · unknownLEFT WING UPPER SIDE STA XORS 103 FOUND BONDED REPAIR PANEL P/N ARC0340. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0971Repair · unknownLEFT WING UPPER SIDE STA XORS 402 JUST FWD OF I/B AILERON FOUND BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0970Repair · unknownLEFT WING UPPER SKIN STA XORS 180 FOUND BONDED REPAIR PANEL P/N ARC0269. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0969Repair · unknownLEFT WING UPPER SIDE STA XORS 403 JUST FWD I/B AILERON FOUND BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0968Repair · unknownLEFT WING UPPER SPOILER NR 1 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0967Repair · unknownLEFT WING SPOILER NR 2 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0966Repair · unknownLEFT WING SPOILER NR 4 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0965Repair · unknownLEFT WING SPOILER NR 5 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0964Repair · noneRIGHT WING NR 3 SPOILER UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0963Repair · noneRIGHT WING SPOILER NR 4 UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010
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