N972FD
Service difficulty reports · 105
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 = 'N972FD' 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 = 'N972FD' 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 FDEA202502030171Crease Beam · crackedMAIN CABIN STA 1020 RH CREASE BEAM IS CRACKED IN 3 SPOTS AROUND HOLE. CUT / TRIMMED DAMAGE SECTION OF CREASE BEAM INNER CHORD FROM STA 1010 TO ORIGINAL SPLICE AT STA 1040 RBL 64.50 AND INSTALLED REPAIR PARTS BETWEEN STA 1004 TO ORIGINAL SPLICE AT STA 1040SDR FDEA202407241048Transmission · failedTE FLAP DISAGREE WHEN TRANSITIONING FROM FLAPS 20 TO 25. RAN QRH, LANDED UNEVENTFULLY. EWR FIM: 27-51-808 DEBRIEF CREW TE FLAPS WILL NOT GO TO 25 AT WHICH POINT THEY GOT A FLAP DISAGREE.CYCLED FLAPS FROM 0 TO 30 NO FAULTS NOTED,BITE ALL 3 FSEU NO FAULTS SDR FDEA202407090976Battery Pack · no testHALF OF INTERIOR EMERGENCY LIGHTS ARE INOP DURING TEST. REMOVED AND REPLACED RIGHT EMERGNCY LIGHT BATTERY PACK.SDR FDEA202406110791Lamp · failedEMERGENCY LIGHT 'UNARMED' LIGHT INOP. RELAMPED AND OP'S CHECKED GOOD IN REF TO 757 MM 33-16-02-2.SDR FDEA202404090452Warning Message · illuminatedON APPROACH WHEN SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE MESSAGE. DISCONTINUED APPROACH AND COMPLIED WITH THE QRH. MESSAGE CLEARED. LANDED FLAPS 20. PER FIM 27-51 FAULT TREE 805, PERFORMED BITE PROCEDURE ON FSEU 1 & 2, ON FSEU 1 FOUND FLAP DISAGRESDR FDEA202310111740Window · failedIN FLIGHT, R FWD WINDSHIELD ELECTRICAL ARCING LOWER HEATING ELEMENT. REPLACED FIRST OFFICER WINDOW #1 PER MM 56-11-01-4 . ALL TEST OK , A/C READY FOR FLIGHT .SDR FDEA202305171059Skin · burnedL/H STRUT OUTBD HAS SIGN OF BURNT AT PPS. 174.3 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.Z # F-5450-T0374528 L/H STRUT STRUCTURE - OUTBOARD SIDE SKIN PANEL - BURN DAMAGE MAJOR REPAIRSDR FDEA202305161060Flap · chafedR/H WING OUTBD FLAP CHAFFED ON UPPER SIDE NEAR SPOILER #10 PERFORMED TRAILING EDGE FLAP NOSE SKIN REPAIR - AREA ADJACENT TO A NOSE RIB, PER SRM 57-53-01-2R, REPAIR 3, FIG. 201 SEE FEDEX E.A F-5750-T0374851 FOR TRACKING. MAJOR REPAIRSDR FDEA202305160979Slat · damagedR/H WING SLAT #5 HAS HOLE ON CLOSURE PANEL INBD SIDE PERFORMED REPAIR FOR MENTIONED CLOSURE PANEL PER SRM 51-70-07 , REF SRM 57-43-01-2R,REPAIR 10, PARAGRAPH 4.C. REP. DIM.: 3" X 1.5". REP. LOC.: 9" FROM O/B. REV. 138.1REPAIR MATERIALS: P/N: BMS 5-101/129 ,SDR FDEA202305151058Panel · crackedAFT CARGO COMP. DURING INS L/H SIDE FLOOR PANEL FOUND CRACK AT STA 1240 DAMAGED PART REMOVED AND NEW PART P/N FX-146N5391-143 (SIDE PANEL) INSTALLED PER SRM 51-40-02SDR FDEA202305151057Panel · crackedAFT CARGO COMP. DURING INS L/H SIDE FLOOR PANEL FOUND CRACK AT STA 1380 DAMGED PART REMOVED AND NEW PART P/N FX-146N5391-147 (SIDE PLATE) INSTALLED PER SRM 51-40-02 MAJOR REPAIRSDR FDEA202305110869Unknown · unknownPDIS 972 31-10 9383 11MAY23 VIE FACT U EMERGENCY LIGHTS PLASTIC ANNUNCIATION LIGHT COVER FELL OFF DURING SHUTDOWN CHECKLIST. COULD NOT LOCATE ALL PARTS IN COCKPIT FACT 11MAY23 05:37 VIE U AMM 311000 LENS ASSY REINSTALLEDSDR FDEA202211122760Bulb · inoperativeEXTERIOR EMERGENCY LIGHT (SLIDE LIGHT) DOOR 1R INOP. BULB REPLACED ACC AMM 33-51-06-2-1 (REV 130.5). OPS TEST SATIS.SDR FDEA202210242676Steering Sys · unknownAIRCRAFT PULLING LEFT DURING MOVEMENT IN ALL PHASES OF GROUND OPS. INSPECTED STEERING ACTUATOR AND LINKS IAW AMM 32-51-00-0 WITHOUT ANY DEFECT FOUND. PERFORMED STEERING TENSION IN THE CABLES NWSA / NWSB / NGPPA AND NGPPB IAW AMM 32-51-00-5-3 WITHOUT ANY SDR FDEA202203140511Latch · brokenHAZCAN FIRE EXTINGUISHER COMPARTMENT LATCH BROKEN. OIL 14MAR22 15:28 BSL U NO RESTRICTION - ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 26-20-1 LATCH FOR DG FIRE EXTINGUISHERS COMPARTMENT INOP. RE STRICTIVE NEF: N ITEM DEFERRED PESDR FDEA202112310777None · noneL/H SLIDE LIGHT INOP. RELAMPED BULB, OPS CHECK NORMAL REF AMM 33-51-06-2-1SDR FDEA202112223121Transmitter · failedPDIS 972 27-50 7959 22DEC21 CGN FACT U TE FLAP ASYM ILLUMINATED WHEN FLAPS 1 WAS SELECTED. FOLLOWED QRH 9.1.14 LANDED AT 162 KIAS WITH NO ISSUES. PART 22DEC21 19:33 CDG U IDENTIFIED PARTS FLAP POSITION TRANSMITTER MPN: 18-1969-18 SDR FDEA202108222070Strut · damagedDURING C CHECK FOUND BURN DAMAGE ON RH SIDE OF NR 2 PYLON INSTALLED DOUBLER REPAIR PER EA F-5450-T0363070P1.SDR FDEA202107261863Seat Track · corrodedFOUND CORROSION ON SEAT TRACK CROWN AT STA 1630 RBL 24.5 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R OPTION 1 FIG 201SDR FDEA202107261862Seat Track · corrodedFOUND CORROSION ON SEAT TRACK CROWN AT STA 1640 LBL 48 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R OPTION 1 FIG 201SDR FDEA202107261861Seat Track · crackedFOUND CRACKED SEAT TRACK FLANGE BETWEEN STA 1580-1600 LBL 58.22 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52 2R OPTION 1 FIG 201SDR FDEA202103090604Lever · dirtyPDIS 972 32-30 7160 09MAR21 CDG FACT U LOGPAGES:3301344 "GEAR DISAGREE" ON SHORT FINAL. GO AROUND AND FOLLOWED QRH PROCEDURES TO A NORMAL LANDING NO INDICATIONS ON SECOND APPROACH SHGN 09MAR21 00:51 CDG U BIT PSEU AS PER FIM 32-09-03/101 SDR FDEA202101130088Trim System · intermittentRUDDER TRIM BECOME INOPERATIVE INFLIGHT STUCK AT 2 DEGREES LEFT. COULD NOT DUPLICATE ON GROUND. PERFORMED RUDDER TRIM SYSTEM TEST, IAW AMM 27-21-00-5-1. TEST SATISFACTORY, RUDDER TRIM SYSTEM OPERATES NORMALLY. AIRCRAFT OK TO CONTINUE.SDR FDEA2020082091942Cylinder · dischargedDURING REMOVAL OF R1 SLIDE FOUND R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE DISCHARGED. R & R THE EMERGENCY POWER RESERVOIR CYLINDER IAW MM 52-11-30-4, CHECKED OK, .ACFT OK FOR SERVICE.SDR FDEA2020081871919Bottle · out of limitsR1 DOOR SLIDE INFLATION CYLINDER PRESSURE OUT OF LIMITS. R & R THE R1 DOOR SLIDE IAW AMM 25-66-01-4.SDR FDEA2020071081481Skin · damagedDURING WALK AROUND, FOUND HOLE ON RIGHT AFT NAVIGATION LIGHT ACCESS DOOR AT LOWER PART. R & R THE RT WING WING TIP AFT ASSY IAW MM 57-31-01-4, ALL CHECKED OK.SDR FDEA2020031290507Light · inoperativeMDIS 972 33-50 6132 09MAR20 MXP FACT U LH SLIDE EMERGENCY LIGHT L25 FOUND INOP. LH SLIDE EMRGENCY LIGHT L25 LAMP (P/N 767) REPLACED IAW AMM 33-51-06-2-1. OPS CHECK SATIS. A/C OK FOR SERVICE.SDR FDEA201907081508Floor Panel · damagedFLOOR PANEL B/S 333.45-377.45 LBL 08-55 DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A ALLOWABLE DAMAGE TABLE 1 REPAIR AS REQD. REPAIRED IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 1.SDR FDEA201907081507Floor Panel · damagedFLOOR PANEL B/S 365-377 B/L 0- RBL 13 DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A ALLOWABLE DAMAGE TABLE 1 REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 1.SDR FDEA201907081506Floor Panel · damagedFLOOR PANEL B/S 365-377 RBL 15-24.75 DAMAGED OUTSIDE PERMITTED LIMTS IAW SRM 53-00-50-1A ALLOWABLE DAMAGE TABLE 1 REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.SDR FDEA201907081505Floor Panel · damagedFLOOR PANEL B/S 297-310.5 RBL 42-62 DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-00-1A ALLOWABLE DAMAGE TABLE 1, REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.SDR FDEA201907081503Floor Panel · damagedFLOOR PANEL B/S 310.5-324 RBL 42-62 IS DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A ALLOWABLE DAMAGE TABLE 1, REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.SDR FDEA201907081502Floor Panel · damagedFLOOR PANEL B/S 297-350 RBL 02-42 DAMAGED OUTSIDE PERMITTED LIMITS IAW 53-00-50-1A ALLOWABLE DAMAGE TABLE 1 REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.SDR FDEA201907081501Floor Panel · damagedFLOOR PANEL B/S 324-365, BL 0-RBL 62 IS DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE TABLE 1, REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 1.SDR FDEA201907081500Floor Panel · damagedUPPER DECK FLOOR PANEL DAMAGED B/S 365-377 RBL 26-44 IS DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 51-00-50 -1A TABLE 1 REPAIR AS REQD. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 1.SDR FDEA201906241539Strap · damagedAGING AIRCRAFT MAIN DECK BS 377.7 LBL 24.75 STABILIZER STRAP REPAIR. REPAIR REPLACED IAW EA #F-5310-T0348004 P1 AND SRM 53-00-51 REPAIR 12.SDR FDEA201906201540Skin · dentedRT ELEV HAS A DENT ON TOP MIDDLE SURFACE REPAIRED THE DAMAGED UPPER PANEL OF THE RT ELEVATOR PER SRM 55-20-01-0I IDENTIFICATION 1, SRM 55-20-01-2R REPAIR 1 AND SRM 51-70-03-0G GENERAL WITHOUT DEVIATION.SDR FDEA201906191529Skin · dentedDENT ON FUSELAGE SKIN AT B/S 522, 1" BELOW STR 26L DENT MEASURED AND EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A, REV 127 FIG 101 DET III, CARRIED OUT REPAIR IAW EA #F-5330-T 347883 P1 .TITLE:FUSELAGE - PLATES & SKINS -DENT AT BSTA522,1" BELOW STR26SDR FDEA201906191525Strip · corrodedRT ELEV O/B AFT END CAP STRIP BULGING. FABRICATED AND REPLACED PARTS IAW GMM 7-0-1001 AND DRAWING#183N2006 AND 183N2007 AND IAW SRM 51-40-02.SDR FDEA201906191523Strip · corrodedLT ELEV O/B AFT END CAP STRIP BULGING. FABRICATED AND REPLACED PARTS IAW GMM7-0-1001 AND BOEING DRAWING# 183N2006 AND 183N2007 AND IAW SRM51-40-02.SDR FDEA201906191489Sleeve · crackedENG #2 I/B T/R SLEEVBE CRACKED AT LOWER CORNER OF CUTOUT FOR BLOCKER DOOR #10 REPAIRED CRACKE ON ENGINE #2 LT T/R SLEEVE INNER PERFORATED SKIN AT THE BLOCKER DOOR#10 IAW EA #:F-7830-T0347748 P1. TITLE ;EXHAUST SYSTEM-TRUST REVERSER GEN- CRACK ON 2L TRANSLATINSDR FDEA201906191478Bracket · crackedRT O/B AFT FLAP, O/B AUX TRACK FAIRING BRACKET IS CRACKED REPLACED RT O/B AFT FLAP O/B AUX TRACK FAIRING BRACKET IAW SRM 51-40-02 AFTER FABRICATION OF NEW BRACKET IAW DRAWING# 113N3333 AND GMM-7-0-1001.SDR FDEA201906181532Panel · crackedSLAT #5 LOWER TRAILING EDGE SKIRT IS CRACKED. REPAIRED THE DAMAGE SLAT #5 LOWER FLEX PANEL PER SRM 57-43-02-2R, SRM 57-43-01-0I IDENTIFICATION 1, SRM 57-43-01-2R REPAIR 10 AND SRM 51-70-07-0G GENERAL AND PARAGRAPH 5(H). REPAIR 10, PARA 4(C) WITHOUT DEVITION.SDR FDEA201906181522Panel · crackedSLAT #6 LOWER TRAILING EDGE MIDDLE SKIRT IS CRACKED. REPAIRED THE DAMAGED SLAT #6 LOWER FLEX PANEL PER SRM 57-43-02-2R, SRM 57-43-01-0I IDENTIFICATION 1, SRM 57-43-01-2R REPAIR 10 AND SRM 51-70-07-0G GENERAL AND PARAGRAPH 5(H) . REPAIR 10, PARA 4(C) WITHOUT DESDR FDEA201906181511Bracket · damagedAFT CARGO DOOR AFT SIDE SEAL DEPRESSOR LOWER CORNER BRACKET IS DAMAGED FABRICATED NEW BRACKET IAW DRAWING#140N2791 REV.B AND GMM 7-0-1001 REV.156. P/N 2024T0-0402, B/N 0191818482, HEAT TREATMENT CERT # HT-19-077. BRACKET P/N:140N2791-9 AND INSTALLED IAW SRM SDR FDEA201906141538Strap · damagedAGING AIRCRAFT MAIN DECK BS 365.25 LBL 24.75 STABILIZER STRAP REPAIR. REPAIR REPLACED IAW EA # F-5310-T0348004 P1 AND SRM 51-00-51 REPAIR 13.SDR FDEA201906141537Strap · damagedAGING AIRCRAFT MAIN DECK BS 365-.25 LBL 45..50 STABILIZER STRAP REPAIR. REPAIR REPLACED IAW EA #F-5310-T0348004 P1 AND SRM 53-00-51 REPAIR 12.SDR FDEA201906051228Transceiver · malfunctionedRADAR NOT GIVING ACCURATE INFORMATION REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 066-50008-0406 POS: ONL SRL: 12218 TAG NBR: 2611E0 ON MPN: 066-50008-0406 CPN: 3414883 SRL: RTA4B-20922 SDR FDEA201905101024Latch · failedDURING POST FLIGHT CHECK FOUND LATCH ON, LAVATORY ACCESS DOOR, BENEATH SINK BROKEN. IN REF TO DISC. 25-40/5348 PREVENTIVELY SET LAV TO INOP RELEASED FOR SERVICE PER MEL : 25-41-01 CATEGORY : C EXPIRATION : 19MAY19 "MEL 25-41-01: LAVATORY WASTE CONTAINER FLAPPSDR FDEA201902010241Leaf Spring · wornTHE LEAF SPRINGS ON THE ESCAPE SLIDE GIRT BAR AT DOOR 1R ARE WORN. REPLACED LEAF SPRINGS IAW SRM 51-40-02 AND REF IPC 25-66-05-05 .
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