N282FE, cancelled Aug 27, 2013
Service difficulty reports · 119
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 = 'N282FE' AND deregistration_id = 'N282FE-2013-08-27' 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 = 'N282FE' AND deregistration_id = 'N282FE-2013-08-27' 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 FDEA201011174409Actuator · failedNR7 LED WOULD NOT RETRACT ON CLIMBOUT. RAN QRH AND IT WOULD NOT CLEAR. REPLACED THE NR 7 SLAT ACTUATOR WITH AND OVERHAULED UNIT PER MM 27-81-032-4. OPS CHECK AND LEAK CHECK GOOD. LEAK AND OPS CHECK NORMAL PER MM 27-81-032-4.SDR FDEA200903070860Skin · dentedWING STATION 544 NR 6 SLAT L/E SKIN HAS LARGE DENT. EVALUATED DENT & FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 2, CUT-OUT DAMAGE & FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2 AND INSTALLED IAW SRM 57-50-3 FIG 1 SDR FDEA200903020788Spar · looseNR 8 RIGHT WING FALSE SPAR LOWER CHORD ABOVE MLG HAS LOOSE FASTENERS AND FOUND CRACKED. REPAIRED IAW STANDARD REPAIR DRAWING SR27-57-038 REV. C.SDR FDEA200902270760Angle · crackedLEFT WING T/E BELOW NR 7 SPOILER HAS CRACKED ANGLE AT FALSE SPAR LOWER CHORD. REPAIRED IAW STANDARD REWORK DRAWING SR27-57-038 REV. C.SDR FDEA200902270759Structure · misrepairedFASTENERS WITH IMPROPER ED STA 460 STR 27L IN MCD DOUBLER. REMOVED FASTENERS FROM AREA FOR ACCESS IAW SRM 51-30-2. TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3 FIG. 1A. FABRICATED DOUBLER & FILLERS IAW SRM 53-30-3 FIG 1A. TREATED AND PRIMED IAW SRM 51-10-2. INSTSDR FDEA200902270758Frame · puncturedFORWARD CARGO AREA BS 540 STR 22L HAS PUNCTURED FRAME. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG. 1. FABRICATED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1.SDR FDEA200902270757Bulkhead · crackedRT WHEEL WELL BS.870 BULKHEAD WEB CRACKED IN 2 PLACES AT LOAD CONTROL VALVE CUTOUT RBL10-16. CUT-OUT DAMAGE AREA IAW SRM 53-10-9 FIG 5. C/W HFEC INSP OF CUT-OUT EDGE IAW NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. CAD PLATED REPAIR PARTS IAW SRM 51-10-6. SDR FDEA200902270753Attach Bracket · crackedNR 8 SLAT ACTUATOR INBD AND OTBD ATTACH BRACKET INSIDE PLATES ARE CRACKED. REMOVED I/B & O/B BRACKETS AT NR 8 SLAT ACTUATOR IAW EA 7-5750-126801 AND SRM 51-30-2 AND S.B. B727-57-0130. FABRICATED 2EA. STEEL DOUBLERS AND 2EA. WEBS IAW EA 7-5750-126801 AND S.B. SDR FDEA200902270750Skin · crackedLEFT WING T/E OUTBD AILERON INBD EDGE LOWER SKIN CRACKED AND BENT WBL 492.0. TRIMMED OUT DAMAGE IAW SRM 51-10-1 & 57-50-1 FIG 4. CW HFEC AND NO CRACKS INDICATED, MATERIAL LOSS 0.100 IN LENGTH & FOUND WITHIN LIMITS IAW SRM 57-50-1 FIG 4. TREATED & PRIMED ESDR 08FDEA00141Module · failedPRESSURIZATION LOSS AT FL230, CABIN ALT 10,000' DESCEND TO (FL)10,000' PSID 0 (ZERO) LOSS OF HEAT. ACFT HARD TO HEAT ON GROUND. OUTFLOW VLV INDICATED CLOSED BUT DID NOT RESPOND IN "MAN D.C.". FOUND SMOKE CONTROL SWITCH ON P4-78 PANEL STUCK IN THE "ON" POSSDR 07FDEA03258Actuator · failedCLIMBING THRU FL190 A/P CRUSE TRIM WOULD NOT WORK IN EITHER DIRECTION, NOR WOULD THE MAIN ELC TRIM WORK IN THE NOSE DOWN DIRECTION. RECYCLED THE CUTOUT SWITCHES, BUT STILL DIDN'T WORK. NO STAB TRIM C/B'S WERE POPPED ON THE DESCENT THE TRIM STARTED TO WORK SDR 07FDEA01733Electrical Sys · contaminatedAT ROTATION, ESSENTIAL POWER FAIL LIGHT CAME ON MOMENTARILY THEN WENT OUT WITH NR 1 GENERATOR FAIL. UNABLE TO BRING NR 1 BUSSSM20ACD200A2 ON LINE. LOST THE FOLLOWING: CAPT'S INST LIGHTS, PITCH TRIM, ASYM FLAPS, NR 1 EPR WITH PACKS TRIPPED, NR 1 OIL TEMP WESDR 06FDEA03587Switch · malfunctionedNR 5 LEADING EDGE FLAP WOULD NOT RETRACT. FLAP RETRACTED NORMALLY. PROBLEM IS WITH INDICATION. REPLACED NR 5 L/E FLAP SWITCH PER MM 27-82-001-4. OPS CHECKS NORMAL OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 40174.SDR 06FDEA03381Window · damagedUPON REMOVAL OF F/O'S NR 1 WINDOW, FOUND UPPER O/B FASTENER HOLE TO BE ELONGATED. FOUND HOLE AT UPPER O/B CORNER OF F/O'S NR 1 WINDOW TO BE OUT OF LIMITS. REPAIRED AREA AS PER FED-EX EA 7-5330-100586. MAJOR REPAIR.SDR 06FDEA03380Skin · misrepairedEXISTING EXTERNAL DOUBLER REPAIR ON PNEMUATIC GROUND SERVICE CONNECTION AFT LT CUT OUT. (DOT 16) REPAIR REQUIRES EVALUATION FOR MAJOR.MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. UPON INVESTIGATION FOUND REPAIR NOT TO BSDR 06FDEA03338Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 9" BY 11" AT STA 1322, LT STRINGER 24, DOT NR 19. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED EXISTING DOUBLER PER SRM 53-30SDR 06FDEA03316Frame · gougedFRAME I/B CHORD GOUGED IN RADIUS STA 950E STR 26R. REMOVED DAMAGE I/B FRAME CHORD BS 950E STR 26R REPAIRED IAW SRM 51-40-4.SDR 06FDEA03315Stringer · gougedFOUND STRINGER 23L AT BS 1324 HAS GOUGE IN LWR SIDE OF STR CHANNEL. REPAIRED STR PER SRM 53-10-3, FIG. 1.SDR 06FDEA03268Shear Tie · damagedFOUND SHEAR TIE, BS 1323, BELOW STR 23L TO HAVE ENLONGATED HOLE.SDR 06FDEA03258Inlet · unknownEXISTING EXTERNAL DOUBLER REPAIR APPROX 6 1/2" BY 6" ON NR 2 ENGINE NOSE INLET LT SIDE. (DOT 32) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED NR 2 ENGINE LT AND RT NSDR 06FDEA03245Depressor · damagedNR 2 CARGO DOOR UPPER FWD SEAL DEPRESSOR CHAFED. REMOVED AND REPLACED NR 2 CARGO DOOR UPPER FWD SEAL DEPRESSOR IAW SRM 51-30-2, 51-30-5 AND 51-30-8.SDR 06FDEA03244Frame · damagedFUSELAGE UPPER LOBE, DRILL START IN FRAME FWD SIDE, 3.5" BELOW STR 8L, BS 720E. REMOVED DRILL START IN FRAME FWD SIDE 3.5" BELOW STR 8L BS 720E AND REPAIRED IAW SRM 51-40-3 FIG 1.SDR 06FDEA03243Stringer · misrepairedEXISTING STRINGER REPAIR AT STA 540, RT STRINGER 7. (DOT 48) REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING STRINGER REPAIR AT BS 540 WAS NOT INSTALLED EPR FAA APPROVED DATA. REMOVED EXISTINSDR 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 06FDEA03241Shear Tie · unknownAFT CARGO BAY FRAME SHEAR TIE STA 950E BETWEEN STR 28L - 29L. REPAIRED SHEAR TIE BETWEEN STR 28L-29L BS 950E IAW SRM 53-10-4, 53-10-1.SDR 06FDEA03229Frame · damagedEXISTING FRAME REPAIR AT STA 700, RT STRINGER 24 (DOT NR 43). REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS FOUND NOT TO BE IAW SRM. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER I.ASDR 06FDEA03228Structure · chafedRIGHT OVERWING AFT EXIT CHAFING ALONG BOTTOM EDGE. REMOVED DAMAGE ALONG BOTTOM SIDE OF R/H OVERWING EXIT AND REPAIRED IAW SRM 52- 00-2 FIG. 2.SDR 06FDEA03189Shear Tie · corrodedFOUND CORROSION C53-111-01 AFT CARGO BAY FRAME SHEAR TIE STA 950F BETWEEN STR 28L - 29L. REMOVED CORROSION ON SHEAR TIE STA 950F BETWEEN STR 28L-29L AND REPAIRED IAW SRM 53-10-1.SDR 06FDEA03164Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP CRACKED AT BS 680 STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03163Stringer Clip · gougedFUSELAGE UPPER LOBE, STRINGER CLIP GOUGED AT BS 660 STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03162Rib · chafedVERT STAB RT AND LT FIN STA 55.9 PANEL SUPPORT RIB CHAFED. BLENDED DAMAGE, OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED PER FED EX EA 7-5530-100583.SDR 06FDEA03165Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT STA 1070, RBL 10 - RBL 65, DOT NR 47. REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR WAS FOUND NOT TO BE ACCOMPLISHED PER FAA APPROVED DATA. REMSDR 06FDEA03139Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 9" BY 9" AT STA 685, BETWEEN RT STRINGER 20 AND 21. (DOT #6) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION A AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMING REPLACED EXISTING REPAIR DOUSDR 06FDEA03141Skin · crackedNR 2 ENGINE INLET INTERIOR SKIN IS CRACKED AT TE 12 O`CLOCK. REPARIED NR 2 ENGINE INLET SKIN PER SRM 54-10-3.SDR 06FDEA03136Skin · damagedN01183 EXISTING EXTERNAL DOUBLER REPAIR APPROX 5 INCH X 10 INCH AT STA. 1155, BETWEEN RT STRINGER 29-30 (DOT NR 22) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED EXISTING EXTERNALSDR 06FDEA03135Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 1070 BETWEEN STR 26L AND 27L UPPER SURFACE. CUT OUT DAMAGE ON FRAME AT BS 1070 BETWEEN STR 26L & 27L LOWER SURFACE AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3.SDR 06FDEA03129Frame · chafedFOUND MAIN CABIN 1130 FRAME IS CHAFED AT STR 5L. REPAIRED FRAME AT BS 1130 STR 5L IAW SRM 51-40-3.SDR 06FDEA03128Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, CRACK IN STRINGER CLIP, STR 7L, BS 720A. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 7L IAW SRM 51-30-2 AND SRM 51-30- 5.SDR 06FDEA03127Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, STR 7R, BS 660. REMOVED AND REPLACED STR CLIP BS 660 STR 7R IAW SRM 51-30-2 AND SRM 51-30-5.SDR 06FDEA03126Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, STR 7R, BS 680. REMOVED AND REPLACED STRINGER CLIP AT BS 680 STR 7R IAW SRM 51-30-2 AND SRM 51-30-5.SDR 06FDEA03125Stringer Clip · corrodedFOUND FUSELAGE UPPER LOBE, STRIGNER CLIP CORRODED, STR 8R, BS 720A. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 8R IAW SRM 51-30-2 AND SRM 51-30- 5.SDR 06FDEA03124Frame · dentedFOUND FWD CARGO BAY FRAME IS DENTED 2 PLACES BS 680 STR 23L AND STR 24L. REMOVED DAMAGE AND REPAIRED DENTED FRAME AT BS 680 STR 23L AND 24L IAW SRM 51-40- 3.SDR 06FDEA03123Frame · gougedAFT CARGO BAY FRAME GOUGED AT BS 950E STR 25L UPPER SURFACE. REMOVED AND REPLACED GOUGED FRAME SPLICE AT BS 950E STR 25L IAW SRM 51-20-1 AND 51-30-2.SDR 06FDEA03122Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, BS 720E, STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 720E STR 7R IAW SRM 51-30-2 AND SRM 51- 30-5.SDR 06FDEA03121Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED BS 720D, STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 720D STR 7R IAW SRM 51-30-2 AND 51-30-5.SDR 06FDEA03070Stringer · crackedFUSELAGE UPPER LOBE, STRINGER IS CRACKED AT FWD SIDE OF WING ILLUMINATION LIGHT, STR 15R, RB 720B PLUS 4.5". REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED. ALL WORK DONE IAW SRM 53-10-3.SDR 06FDEA03071Stringer · crackedFUSELAGE UPPER LOBE, CRACK IN STRINGER FWD OF WING ILLUMINATION LIGHT, STR 15L, BS 720B PLUS 3.5. COMING FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-3.SDR 06FDEA03069Stringer · crackedFUSELAGE UPPER LOBE, CRACK IN STRINGER AFT OF WING ILLUMINATION LIGHT STR 15L, BS 720B PLUS 15. REPAIRED STRINGER PER SRM 53-10-3, FIG 5.SDR 06FDEA03073Skin · damagedEXISTING FLUSH REPAIR APPROX 3" BY 2 1/2" AT STA 645, RT STRINGER 22. (DOT #5) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMING FOUND REPAIR NOT TO BE FAA APPROVED DATA. REPAIRED PESDR 06FDEA03072Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 12" BY 16" AT STA 1120-STA 1132, BETWEEN LT STRINGER 29 AND RT STRINGER 29 (DOT #23) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ADDED FASTENERS
Back to N282FE, cancelled Aug 27, 2013