N265FE, cancelled Mar 1, 2013
Service difficulty reports · 87
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 = 'N265FE' AND deregistration_id = 'N265FE-2013-03-01' 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 = 'N265FE' AND deregistration_id = 'N265FE-2013-03-01' 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 FDEA201208243149Oxygen Bottle · lowPERFORMED TRANSIT CHECK. PORTABLE CREW OXYGEN BOTTLE LOW. REQUIRES REPLACEMENT. R & R FLIGHT CREW PORTABLE OXYGEN BOTTLE OPS NORMAL IAW MM35-30-000-0-0. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R FLIGHT CREW PORTABLE OXYGEN BOTTLE OPS NORMAL IAWSDR FDEA201111295075Transmitter · malfunctionedOTBD FLAP ASYMMETRY WHILE ON APPROACH. LT FLAP BY 20DEG, RT FLAP AT 15DEG. REMOVED AND REPLACED LEFT OUTBOARD FLAP POSITION TRANSMITTER ASSY AND CABLE. IAW MM 27-52-013-4 AND MM 27-52-013-5. ADJUSTED AND OPS CHECKED GOOD.SDR FDEA201012284757Controller · malfunctionedON TAKEOFF CLIMB AT 400'AGL, AT CLIMB POWER, EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. ENGINE ANTI-ICE WAS OFF, THE ENGINE RECOVERED AFTER A COUPLE OF BANGS, ALL ENGINE PARAMERTERS WERE NORMAL DURING CLIMB. WE OBSERVED NO OTHER ENGINE PARAMETERS DUSDR FDEA201007192596Structure · crackedRT WING, INBD FLAP, MID FLAP, AFT CHORD IS CRACKED AT WBL 112. CUTOUT SECTION CHORD CRACKED AT RT WING INBD FLAP MIDFLAP WBL 112 DIM: 47.6250" IAW SRM 51-40-4, FIG 1 AND FABRICATED SECTION CHORD FROM BAC 1503100046 7075T6 DIM: 47.6250 " & SPLICE DIM: 8.5" IAW SDR FDEA201007162566Skin · gougedSURROUND INNER SKIN GOUGED STA 620 STR 16L, CUT OUT DAMAGED AREA DIM APPROX 2" X 1" AND 1" X 1.2". FABRICATED DOUBLER REPAIR FROM 2024-T3 .125, DIM APPROX 9.50" X 4" AND FILLERS FROM 2024-T3, .125 DIM APPROX 2"X .950 AND 1.20" X .950 AND INSTALLED DOUBLER ANSDR FDEA201007152534Web · corrodedLH W/W CORROSION ON WEB AT STRINGER 18A FROM BS 920 TO 930 REMOVED SILL (WEB SHELF ON STRINGER 18A) AT BS 870 TO BS 950 LBL 55, FABRICATED SILL (WEB) FROM 7075O .080 DIM: 8.5" X 65.4, HEAT TREATMENT INSP 7075O TO T6 CONDITION IAW FASI REPORT 2-37153-801 REV A,SDR FDEA201007152556Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 990 BETWEEN STRINGERS 29L AND 28L CUT OUT DAMAGED SECTION OF SHEAR TIE 1" X 6" IAW FED SRM, REV 103, 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR USING 7075-0, .080" X 6" X 8.5" IAW SRM 53-10-4, FIG 15. INSTALLED SHEAR TIE REPAIR ISDR FDEA201007142561Skin · gougedSURROUND INNER SKIN GOUGES STA 640 STR 16L COMPLIED WITH EA 7-5330-135570 FUSELAGE AD 98-11-03 R1, SURROUND STRUCTURE, INNER SKIN GOUGE REPAIR BY BLENDING GOUGES IAW SRM 727 51-10-01 AND EA 7-5330-135570 AND FOUND WITHIN LIMITS EA 7-5330-135570.SDR FDEA201007132504Stringer · corrodedCORROSION ON STRINGER 27L FROM BS 950A TO 1130. REMOVED SECTION OF STRINGER 27L FROM BS 950D PLUS 10 INCHES TO BS 1005, 85 INCHES LONG IAW SRM, REV 103, 53-10-3 FIG 1. FABRICATED STRINGER SECTIONS USING BAC 1498-147, 7075-T6, 19 INCHES LONG, 20 1/2 INCHES LSDR FDEA201007132500Stringer · corrodedCORROSION ON STR 28L AT STRINGER SPLICE BS 1015.SDR FDEA201007122492Bulkhead · crackedMAIN CABIN 1183 BULKHEAD SKIN HAS CRACK AT LBL 60, WL 220 REMOVED LINE SUPPORT ANGLE, HORIZONTAL STIFENERS, CUT OUT DAMAGED AREA APPROX. DIM 4.29"X2.4", FABRICATED DOUBLER FROM P/N 2024-T3 .063 DIM 10 3/4" X 10", FABRICATED FILLER FROM P/N 2024T3 .050 DIM 2 3/SDR FDEA201007092441Skin · gougedMCD SURROUND INNER SKIN GOUGED STA 460 STR 5L. REMOVED INNER SKIN BS 460-510 UPPER FWD IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024 T3 .125" PO 90010048 DIM: 48" X 79" IAW DRAWING 53FX2022 REV C. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED FWD UPPER INSDR FDEA201007092464Seat Track · corrodedSEAT TRACK CORRODED MAIN CABIN LBL 45 BS 850-760. REMOVED DAMAGED SEAT TRACK AND "T" CHORD AND FABRICATED NEW SEAT TRACK FROM BAC 1520-3417178T6 AND NEW "T" CHORD FROM BAC 1506-1108-7075T6. INSTALLED NEW SEAT TRACK & "T" CHORD ALL IAW DWG 65-16279 & SRM 51-3SDR FDEA201007092440Skin · gougedSURROUND INNER SKIN GOUGED STA 620, STR 5L. REMOVED INNER SKIN 600 TO 640 UPPER AFT IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024T3 .125 DIM 48" X 79" IAW DRAWING 53FX2022. INSTALLED NEW INNER SKIN IAW SRM 51-30-2.SDR FDEA201007092442Skin · gougedSURROUND INNER SKIN GOUGED STA 520, STR 5L. REMOVED MAIN CARGO DOOR INNER SKIN CENTER AREA IAW SRM 51-30-2. FABRICATED CENTER INNER SKIN USING 2024 T3 .090" PO 2011153 DIMENSIONS 88" X 34" IAW DWG 53FX2022. TREATED AND PRIMED INNER SKIN IAW SRM 51-10-2. INSTSDR FDEA201007092466Skin · delaminatedRT WING INBD AILERON TAB HAS DISBONDING T/E SKIN SURFACE REMOVED DAMAGED AREA (15.5" X 3.52") SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-00 PARAGRAPH NR 7. FABED FILLER AND DOUBLER ( 15.5" X 3.5") AND DOUBLER (19" X 5.5") FROM 2024T3 .012 IAW SRM 51-40-20 SDR FDEA201007072397Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 970 BETWEEN STRINGERS 30 AND 29R. CUT OUT DAMAGED AREA OF SHEAR TIE AT BS 970 STR 29-30R IAW SRM 53-10-4 FIG 12 DIM 4 1/2" X 3" FABRICATED REPAIR PARTS USING 7075 O .071" DIM 10 1/4" X 7 1/4" 7075T6 .063" DIM 4 1/2" X 2 3/8" ASDR FDEA201007062380Stringer · corrodedCORROSION - STRINGER 27L, STATION 740 INSIDE CHANNEL. CUT OUT STRINGER 27L AT BS 740, 8 5/8" LONG AND 2 STRINGER TIES ANGLES IAW SRM REV 103 53-10-3 FIG 1 51-30-2. FABRICATED STRINGER SECTION FROM BAC1498-147, 7075T6, 8 5/8" LONG SPLICE FROM BAC1498-131 707SDR FDEA201007062371Skin · corrodedCORROSION - UPPER SKIN, EXTERIOR SURFACE OF WING CTR SECTION FUEL TANK. APPROX BS 825, RBL 12. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 57-30-1 FIG 4. REPAIRED AREA IAW EA 7-5730-142035.SDR FDEA201007052391Web · crackedAFT STAIR AREA, RIGHT LOWER TORQUE BOX WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA, DIMENSION 1/4" AFT AIRSTAIR AREA RT BS 1223 IAW SRM 51-40- 2 FIG 1, FABRICATED 2 EA. REPAIR PLATES FROM 2024T3 .040, DIM: 5 1/8" X 1 3/4" IAW SRM 51-40-2 FIG 1SDR FDEA201007052390Web · crackedAFT STAIR AREA, RIGHT LOWER TORQUE BOX WEB CRACKED 2 EA AT LIGHTING HOLE BS 1236. CUTOUT DAMAGED AREA DIM: 1/4" AT AFT AIRSTAIR AREA RH BS 1236 IAW SRM 51-40-2 FIG 1. FABRICATED 2 EA. REPAIR PLATES FROM 2024T3 .040 DIMENSION 4 1/2" X 1 5/8" IAW SRM 51-40-2 FISDR FDEA201007032343Stringer · corrodedCORROSION ON STRINGER 29L FROM BS 950F TO 970. REMOVED CORROSION ON STR 29L FROM 950F TO 970 IAW SRM 51-10-6. CW UT. THICKNESS IAW NDTM 51-00-00 PT 4 FIG 2, ORIGINAL AREA .140, REMAINING .111. EVALUATED AREA FOUND TO BE WITHIN LIMITS IAW EA 7-5330-135567. TRSDR FDEA201003100769Landing Gear · malfunctionedON DEPARTURE RETRACTED GEAR AND RT GEAR DOWN AND RT GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED RED TABS TO NO AVAIL. PERFORMED VISUAL INSP OF THE RT MLG, NO GEAR PIN INSTALLED, NO OBVIOUS DEFECTS NOTED. DEBRIEFED CREW, GEAR DOOR INDICATION WAS CORRSDR 07FDEA04692Frame Splice · crackedFWD LOWER CARGO SPLICE FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 SPLICE FRAME, FABRICATED AND INSTALLED NEW SPLICE FRAME IAW 727 SRM 51-10-01 AND FEDEX DRG 53FX1370.SDR 07FDEA04552Vane · failedCAPT'S STICK SHAKER WENT OFF. A/C WAS PROPERLY CONFIGURED FOR T/O. PULL C/B. REMOVED AND REPLACED AOA VANE. VANE OPS CKS GOOD, REF B727-200MM, RPT BY: 437820. PERFORMED OPS CK OF EGPWS AND FOUND AOA VANE FAULT FOR LAST FLIGHT LEG. PULLED LEVER LATCH C/B SDR 07FDEA02738None · noneAFTER GEAR RETRACTION ON CLIMB-OUT, SYS A HYD ENG NR 1 PUMP LOW PRESS LIGHT ILLUMINATED AND NOTICED HYD SYS A QUANTITY DECREASING. JACKED AIRCRAFT IAW THE B727-200 AMM 07-11-000-2. CYCLED THE LANDING GEAR 15 PLUS TIMES WHILE CYCLING. THE FLT CONTROL NUMEROUSDR 07FDEA02637Hose · failedUPON GEAR RETRACTION AFTER T/O SYS A FLUID QTY WENT TO ZERO. LT MAIN GEAR REMAINED EXTENDED. SYS A PUMPS AND FLUID SHUTOFF SWITCH WERE TURNED OFF FOR APPROX 25 MINS WITH ENGINES RUNNING. GEAR MANUALLY EXTENDED. FOUND RETRACT LINE BLOWN ON LEFT GEAR. REMOVSDR 05FDEA03718Skin · corrodedEXTERIOR FUSELAGE, RAM AIR DOORS ACTUATOR ACCESS PANEL HAS CORROSION ON LANDS BETWEEN STRINGER 28-L AND STRINGER 28-R AT STATION BS 720B. REMOVED CORROSION IAW B727 SRM 51-10-6,ORIGINAL MATERIAL AT AREA .090" MATERIAL REMAINING .053" FOUND OUT OF LIMITS IAW BSDR 05FDEA03452Skin · corrodedFORWARD PIT SKIN CORRODED AT BS 720D BETWEEN STRINGERS 26L AND 27L. REMOVED, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR TO FUSELAGE SKIN AT STA 720D BETWEEN STRINGERS 26L AND 27L ALL IAW FX B727 SRM 53-30-3, 53-20-2 FIG 2, 51-30-2, 51-33-2, SDR 05FDEA03451Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT RT STA 495 AND STRINGER 20R. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ON FUSELAGE EXTERNAL SKIN FROM STA 480 TO 540 FROM STRINGER 20R TO 23R ALL IAW SRM 53-30-1,53-30-2 FIG 2,53-30-3 FIG 3,51-30-2 AND 51-1SDR 05FDEA03412Channel · corrodedLEFT AFT SERVICE DOOR ZEE CHANNEL HAS BARE METAL AND CORROSION AT STRINGER 17L FROM STA 1045 TO 1060. REMOVED AND REPLACED CHORD ANGLE IAW BOEING DRAWING 65-56148 AND FX SRM B727 53-10-8 AND 51-30-2.SDR 05FDEA03048Connector · deterioratedON T/O FROM MSN, PLACED GEAR HANDLE TO UP, GEAR RETRACTED AND ALL LIGHTS EXTINGUSIHED NORMALLY, HOWEVER WHEN THE GEAR HANDLE WAS PLACED TO OFF, THE RED DOOR LIGHT ON FWD PANEL AND RT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. REMOVED THE CANON PLUG FROMSDR 05FDEA01510Actuator · malfunctionedON GEAR EXTENSION FROM OFF POSITION TO DOWN, NLG DID NOT UNLOCK (OR GO GREEN), RECYCLED GEAR HANDLE TO UP, LIGHTS OUT, GEAR HANDLE DOWN, 3 GREEN LIGHTS. REPLACED NOSE GEAR LOCK ACTUATOR IN REFERENCE TO 727-200 AMM 32-33-011-4, OPERATION AND LEAK CHECKED GOOD SDR 05FDEA00354Landing Gear · malfunctionedNOSE GEAR FAILED TO EXTEND WHEN GEAR HANDLE PLACED DOWN RED UNSAFE INDICATION. AFTER 30 SEC NOSE EXTENDED GREEN SAFE INDICATION.SDR MXO2004F00000Bearing · contaminatedWHILE LANDING, THE FLIGHT CREW NOTICED A SHIMMY IN THE LANDING GEAR. BELIEVING THAT THEY HAD BLOWN A TIRE, THEY STOPPED ON A TAXIWAY AND NOTIFIED MAINTENANCE, INSPECTED THE LANDING GEAR. A BLOWN TIRE WAS NOT THE CASE AND MAINT RELEASED THE AC TO TAXI TO RAMPSDR 03FDEA00371Uplock Switch · inoperativeFLIGHT TEST. AIR BORNE WITH GEAR UP AND LDG GEAR HANDLE IN OFF POSITION, RED NOSE GEAR LIGHT COMES ON BRIGHT, AND GREEN NOSE GEAR LT COMES ON DIM. NO OTHER GEAR OR DOOR LIGHTS ON. NO LIGHTS ON S/O PANEL. LOG BOOK ENTRY REQ. UPON TROUBLESHOOTING NLG FOUND SDR 03FDEA00332Frame · crackedFRAME IS CRACKED AT WL 208, BS 1176, LBL 16. BS 1176 FRAME CRACKED AT LBL 16, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1, REMOVED BS 1176 FRAME RBL 65 - LBL 65 WL 208, LOCATED AND BACKDRILLED REPLACEMENT FRAME PER SRM 51-30-5 AND 51-30-8SDR 03FDEA00330Stringer · gougedGOUGE IN STRINGER 3 RT OB FLANGESTA 540. REMOVED & REPALCED STRINGER 3 RT BS 530 TO BS 550 I.A.W. FED EX EA 7-5310-69439.SDR 03FDEA00329Stringer · gougedGOUGE IN STRINGER 3 RT OB FLANGE STA 520. REMOVED & REPLACED STR 3 RT BS 510 TO BS 530 IAW FED EX EA 7-5310-69439.SDR 03FDEA00331Web · corrodedCORROSION ON UPPER SURFACE OF HORIZONTAL WEB INBOARD OF STRINGER 18A, BS 908 RBL 66 WL 189.SDR 03FDEA00327Stringer · crackedSTRINGER END CRACKED AT FASTENER BS 720B PLUS 4 STR 15L. REPAIRED STR 15L BY SPLICING IN NEW REPAIR SECTION STRINGER FROM BS 720A+13, AFT TO LIGHT. REPAIR DONE PER 727 SRM 53-10-3 FIG 1 DETAIL 2.SDR 03FDEA00297Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 500 STR 25L.SDR 03FDEA00298Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 500, BETWEEN STR 23R AND 24R.SDR 03FDEA00299Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 520 STR 24R.SDR 03FDEA00300Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 580 BETWEEN STR 24L AND 25L.SDR 03FDEA00301Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 600, BETWEN STR 24L AND 25L.SDR 03FDEA00302Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 560, BETWEEN STR 24L AND 25L.SDR 03FDEA00303Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 660, BETWEEN STR 24L AND 25L.SDR 03FDEA00304Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 660 STR 24R.SDR 03FDEA00307Frame · dentedDENT IN FRAME, FWD CARGO BAY, BS 520, BETWEEN STR 24L AND 25L.
Back to N265FE, cancelled Mar 1, 2013