N728FD
Service difficulty reports · 266
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 = 'N728FD' AND registry_match = 'registration' 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 = 'N728FD' AND registry_match = 'registration' 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 FDEA201102180630Bulkhead · corrodedFWD CARGO - AFT PRESSURE BULKHEAD ABOUT FRAME 39, FROM STRINGER 50-52R, FOUND EXFOLIATION CORROSION. REPAIRED AS PER SRM 53-15-17, FIGURE 203 REV 74. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 111.SDR FDEA201102180629Skin · crackedLT FIXED T/E PANEL UPPER SURFACE AT APPROX STA 1260, FOUND CRACKED. REPAIRED AS PER SRM 57-51-12 FIGURE 210 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR FDEA201102170597Mount · corrodedNR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE SPOT FACE COROSSION FOUND. NR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE SPOT FACE COROSSION REMOVED IAW SRM 51-74-10, REV 74 AND FOUND WITHIN LIMITS IAW SRM 54-51-81, FIG 104, REV 74. ORIGINAL MATERIAL THICKNESDR FDEA201102170596Mount · corrodedNR 2 ENGINE PYLON FWD MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-74-10 REV 74 AND FOUND EXCEEDED LIMITS PER SRM 54-51-81 FIGURE 104 REV 74. MATERIAL ORIGINAL THICKNESS = 0.780", MATERIAL REMOVED = 0.018", MATERIAL REMAINING SDR FDEA201102170589Arm · crackedAVIONICS COMPARTMENT ACCESS DOOR FOUND LT HINGE ARM CRACKED. REPAIR CARRIED OUT IAW SRM 52-41-14, FIG 201, REV 74. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111. EA 6-5240-147614.SDR FDEA201102160582Skin · misrepairedEXISTING REPAIR FOUND AT LT WING CTR T/E FLAP UPPER SKIN SURFACE EXISTING REPAIR FOUND AT LT WING CTR T/E FLAP UPPER SKIN SURFACE BETWEEN RIB 13 AND RIB 16 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. NEW REPAIR AT LT WING CTR T/E FLAP USDR FDEA201102160569Rib · crackedLT WING INBD T/E FLAP HORIZONTAL UPPER FLANGE OF RIB 25A FOUND CRACKED. CRACKED BRACKET AT RIGHT HAND WING INBOARD TRAILING EDGE FLAP REMOVED AS PER A300-600 SRM 51-40-21 REV 74. NEW BRACKET FABRICATED AS PER DRAWING A57960114 USING 2024-O-0.025" MATERIAL ASDR FDEA201102150567Skin · misrepairedEXISTING REPAIR FOUND AT FRAME 36 STR 32 - 33 LT EXISTING REPAIR ON FUSELAGE EXTERIOR SKIN AT FR 36 BETWEEN STRINGER 32-33 LT EVALUATED AND FOUND NOT IAW APPROVED DATA. NEW REPAIR AT FUSELAGE SKIN AT FR 36, STR 32-33, LT ACCOMPLISHED IAW SRM 53-10-12, FIG 2SDR FDEA201102150568Rib · crackedRIGHT HAND WING INBOARD TRAILING EDGE FLAP HORIZONTAL UPPER FLANGE OF RIB 25A FOUND CRACKED. CRACKED RIB 25A AT THE RIGHT HAND WING INBOARD TRAILING EDGE FLAP HORIZONTAL UPPER FLANGE REMOVED AND REPLACED AS PER SRM 51-40-21 REV 74. REPAIR CLASSIFIED AS MINSDR FDEA201102140564Bulkhead · corrodedAFT PRESSURE BULKHEAD AT LOWER RIM AREA AT FWD FACE OF FR80/82 ABOUT STRINGER 35R TO STRINGER 38R, STRAP PN A53984667208 CORROSION EXCEEDED LIMITS AFT PRESSURE BULKHEAD AT LOWER RIM AREA AT FWD FACE OF FR80/82 ABOUT STRINGER 35R TO STRINGER 38R, STRAP PN A5398SDR FDEA201102040473Engine · oil consumptionNR 1 ENGINE BURNED 1.5 QTS PER HOUR, THE FIRST 2.5 HRS. AIRCREW RECORDED ENGINE READINGS EACH 30 MINUTES IN FLIGHT. THE NR 2 ENG APPEARED NORMAL. MECHANIC SERVICED NR 1 ENGINE (3 QTS ADDED) TO FULL. PERFORMED GVI OF NR 1 ENGINE COWLING, DRAIN MAST AND TAISDR FDEA201001070037Seal · leakingLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, TRIED BOTH SYS. HANDLE WOULD NOT GO PAST NEUTRAL POSITION. RETURNED TO DEPARTURE. FOUND HYD FLUID LEAKING FROM BOTTOM OF RT PITCH DAMPER AND PRESSURE INDICATOR POPPED. R & R RT MLG PITCH DAMPER IAW AMM 32-11-SDR 08FDEA04699Warning Light · false activationAT 250' ON AN ACTUAL CAT3 APPROACH GOT RED AUTOLAND FLASHING LIGHT ALL PARAMETERS APPEARED NORMAL. EXECUTED A GO AROUND. PERFORMED A FAULT ISOLATION PROCEDURE AND A AFS LAND TEST PER AMM 22-42-00-0. NO FAULTS WERE RECORDED ON DISPLAY OR TRIFOLD FAILURE RESDR 08FDEA03405Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 LG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 LG; POTTED EDGES, COMPLETED CURE AND SANDED THE EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED THE PANEL IAW DWG SRZ 25-005, REV "G".SDR 08FDEA03397Rib · crackedRIGHT WING INBD FLAP NOSE RIB NR 5 IS CRACKED AT RIVET HOLE. FABRICATED REPAIR DOUBLER REF SRM 57-50-00; PG 204. ALODINED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7.SDR 08FDEA03395Rib · crackedRIGHT WING INBD FLAP NOSE RIB NR 9 IS CRACKED AT A RIVET HOLE. FABRICATED A REPAIR DOUBLER REF SRM 57-50-00; PG 204. ALODINED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7.SDR FDEA200808083334Floor Panel · damagedCABIN FLOOR PANEL 241 BF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR FDEA200808083333Floor Panel · damagedCABIN FLOOR PANEL 241 MF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03334Floor Panel · damagedCABIN FLOOR PANEL 241 BF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03333Floor Panel · damagedCABIN FLOOR PANEL 241 MF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03349Floor Panel · damagedCABIN FLOOR PANEL 241 EF IS DAMAGED REPAIRED CABIN FLOOR PANEL 241 EF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKISDR 08FDEA03348Floor Panel · damagedCABIN FLOOR PANEL 241 DF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03347Floor Panel · damagedCABIN FLOOR PANEL 242 AJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 AJ BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03346Floor Panel · damagedCABIN FLOOR PANEL 241 AJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 AJ BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SDR 08FDEA03345Floor Panel · damagedCABIN FLOOR PANEL 241 WH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED SDR 08FDEA03344Floor Panel · damagedCABIN FLOOR PANEL 241 CK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SDR 08FDEA03343Floor Panel · damagedCABIN FLOOR PANEL 242 MF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 MF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKSDR 08FDEA03342Floor Panel · damagedCABIN FLOOR PANEL 242 PF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 PF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03341Floor Panel · damagedCABIN FLOOR PANEL 231 EF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 EF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SDR 08FDEA03340Floor Panel · damagedCABIN FLOOR PANEL 242 RJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 RJ BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED SDR 08FDEA03339Floor Panel · damagedCABIN FLOOR PANEL 231 QG IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 QG BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NSDR 08FDEA03338Floor Panel · damagedCABIN FLOOR PANEL 231 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 AH BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED SDR 08FDEA03337Floor Panel · damagedCABIN FLOOR PANEL 242 DK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NSDR 08FDEA03336Floor Panel · damagedCABIN FLOOR PANEL 241 QH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NSDR 08FDEA03335Floor Panel · damagedCABIN FLOOR PANEL 241 GF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 GF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03332Floor Panel · damagedCABIN FLOOR PANEL 262 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 262 AH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03331Floor Panel · damagedCABIN FLOOR PANEL 251 YG IS DAMAGED. REPAIRED CABIN FLOOR PANEL 251 YG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03330Floor Panel · damagedCABIN FLOOR PANEL 251 RT IS DAMAGED. REPAIRED CABIN FLOOR PANEL 251 RT BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03329Floor Panel · damagedCABIN FLOOR PANEL 261 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 261 AH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03328Floor Panel · damagedCABIN FLOOR PANEL 241 KJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 KG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03327Floor Panel · damagedCABIN FLOOR PANEL 242 AK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 AK BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SSDR 08FDEA03326Floorboard · crackedCABIN FLOORBOARD IS CRACKED AT BS 1552, LBL 40. REPAIRED CABIN FLOOR PANEL 231 HG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APSDR 08FDEA03325Floor Panel · crackedCABIN FLOORBOARD IS CRACKED AT BS 1711, LBL 60. REPAIRED CABIN FLOOR PANEL 231 VG DOT C389 BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MASDR 08FDEA03324Floor Panel · crackedCABIN FLOORBOARD AT FRAME C22 - C26, LBL 48 IS CRACKED. REPAIRED CABIN FLOOR PANEL 23 JG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKEDSDR 08FDEA03323Floor Panel · crackedCABIN FLOORBOARD IS CRACKED FROM FRAME C19 TO C22, LBL 24. FABRICATED A NEW PANEL FROM THE OLD PANEL, LOCATED HOLES, COUNTERBORED, POTTED EDGES, CURED POTTING, SANDED THE EDGES, INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW DWG SRZ 25-005; REF G.SDR 08FDEA03322Floor Panel · damagedBROKEN FLOORBOARD AT RBL 72; FRAME 43 TO FRAME 47. REPAIRED CABIN FLOOR PANEL 242 WH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED ANDSDR 08FDEA03310Rib · damagedWHILE ACCOMPLISHING EO 6-5750-7-5000 PT 4 "WINGS - INBD FLAP, REPLACEMENT NOSE RIB 7 RT", STEP 10; THE ACCESS HOLE HAS BEEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. OMITTED FASTENERS AT EXTENDED CUT OUT; INSTALLED OVERSIZED FASTENERS AND PERFORMED SPAR REPAIRSDR 08FDEA03309Skin · damagedWHILE ACCOMPLISHING EO 6-5750-7-5000 PT 3 "WINGS INBD FLAP, REPLACEMENT NOSE RIB 7 LT, STEP 10; THE ACCESS HOLE HAS BEEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. FLAP WAS FOUND TO BE BEYOND TIMELY REPAIR. RECEIVED NEW FLAP REF TAG NR 6934A5. FOR INSTALLSDR 08FDEA03271Rub Strip · wornRIGHT INBD FLAP L/E NOSE SKIN STRAPS HAVE ELONGATED HOLES, (2 STRAPS) MATERIAL ID IAW A300-600 SRM 51-31-00. FABRICATED, LOCATED AND DRILLED IAW A300-600 SRM 51-40-44. ALODINED AND PRIMED IAW A300-600 SRM 51-21-10.SDR 08FDEA03248Seat Track · damagedMAIN CABIN BETWEEN FRAME 63 AND FRAME 64, RBL 18 THE SEAT TRACK IS DAMAGED. SPLICED IN A NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16, FIG 210. ALODINED, PRIMED AND PAINTED IAW A300-600 SRM 51-21-10. APPLIED CIC IAW A300-600 SRM 51-23-20, PARA 9.
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