N33284
Service difficulty reports · 85
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 = 'N33284' 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 = 'N33284' 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 CALA2024080200349Switch · dirtyAUTO THROTTLE SWITCH TEST AND CLEANING {B737-76-3-3265}. ACCOMPLISH WORK CARD 29-7611-1-1001 AUTO THROTTLE SWITCH TEST AND CLEANING. PERFORMED AUTO THROTTLE SWITCH TEST AND CLEANING IAW TASK CARD NO: 29-7611-1-1001. CHECKS GOOD AT THIS TIME.SDR CALA2024070201950Engine · shutdownDUE TO AN IN FLIGHT SHUT DOWN OF THE NO. 1 ENGINE WITH 45 MINUTES OF SUBSEQUENT NO. 1 ENGINE WINDMILLING: ACCOMPLISH AN INSPECTION OF THE NO.1 ENGINE AFTER IN-FLIGHT WINDMILLING REF AMM TASK 71-00-00-210-802-F00. ARMENTA TOMC COMPLETED INSPECTION REF AMM 71-00SDR CALA2024041501083Aoa · faultySPD LIMIT FLAG OCCASIONAL STICK SHAKER ALL ON CAPT SIDE ADI SMYD -1 SHOWS AOA SIG ERROR, T433, MX MESSAGE 27-31004, FIM 27-32 TASK 809. RRD CAPTS AOA SENSOR, AMM 34-21-05. REQUIRES OPS CKS, BONDING CK AND SEALANT. PERFORMED AOA SENSOR TEST, COMPLETE INSTALLASDR CALA2023101103032Shaft · unknown1L OUTSIDE DOOR HANDLE MOVED TO STRAIGHT UP IN FLIGHT SUSPECT HANDLE SHAFT SPRING WORN OUT, REMOVED AND REPLACED HANDLE SHAFT IN L1 DOOR REF AMM 52-11-11-000/400-802. OPS CKS GOOD. PERFORMED REQUIRED RII INSP FOR INSTALL OF L1 DOOR HANDLE SHAFT. REF AMM 52-11-SDR CALA2023070302138Motor · faultySTAB OUT OF TRIM LIGHT ON CLIMB OUT WITH AUTO PILOT ON AND OFF. NO ELEC TRIM. UPDATED WITH PICTURES OF STAB FAULTS CHECKED FOR 115V AT STAB TRIM MOTOR CONNECTOR D700 PIN 1,2,3, TO UPDATE ROTABLE PARTS TAG. PIN 10 HAVE 116V ON ALL 3 NEXT STEP IS TO REPLACE STABSDR CALA2023052401611Landing Light · inoperativeRT RETRACTIBLE LANDING LIGHT INOP RETRACT MOTOR OK, LIGHT RETRACTED, ALL OTHER LANDING LIGHTS OK. PLACED ON MEL REQUEST MEL APPROVED. REMOVED AND REPLACED RT RETRACTABLE LANDING LIGHT REF. AMM 33-42-02-960-801. OPS CHK, GOOD. PLACARD REMOVED PARTS USED: 00-058SDR CALA2023030900667Indicator · inoperativeFLAPS WOULD NOT DELOY PAST 1/ALT FLAPS USED PHOTOS ADDED. LEFT TRAILING EDGE INDICATOR NEEDLE LAGS BEHIND RIGHT INDICATOR REPLACED TRAILING EDGE FLAP POSITION INDICATOR. OPERATION NOW THE FLAP LOCKOUT REPORT FOR THE EVENT IN DFD INDICATES THAT THE ADDING DFDSDR CALA2019112702094Window Frame · crackedCRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 PER AVO # 284-19- 10-26-02 (CRACK CONDITION 1). CRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 HAS BEEN REPAIRED PER EC/RA # 5311-02301. INITIATE A DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO " ACCOMPLISH AN INITIASDR CALA2019112702095Window Frame · crackedCRACK FOUND ON R1 WINDOW FRAME DURING HFEC INSPECTION IAW AVO # 284-19-10-26-02 STEP "B". CRACK FOUND ON R1 WINDOW FRAME DURING HFEC INSPECTION HAS BEEN REPAIRED PER EC/RA 5311-02302. INITIATE A DTA DIP FOR THE R1 WINDOW FRAME REPAIR TO " ACCOMPLISH AN INITIALSDR CALA2019112702090Channel · dentedAFT CARGO COMPARTMENT STA.747 L/H JUST ABOVE THE SIDE PLATE BETW EEN STR24L TO 24L THERE IS A DENT ON THE HAT SECTION. INITIATE A DTA DIP TO -ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRCRAFT REACHING 75,000 TOTAL FLIGHT CYCLES. PLANNIN G TO CONTACTSDR CALA2019112862074Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 157.10 CRACK INDICATION NOTED,9" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56,000 TOTAL COMSDR CALA2019112862073Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 147.90 CRACK INDICATION NOTED, 17" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56,000 TOTAL COMPOSDR CALA2019112862072Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA.101.90 CRACK INDICATION NOTED,20" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW SRM 5510-10- 01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56000 TOTAL CSDR CALA2019111101951Skin · crackedR/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 138.70 CRACK INDICAT ION NOTED, 6" INCHES FROM THE FWD SPAR. REPAIRED R/H HORIZONTAL LWR SKIN CRACK AT STA. 138.10 PER SRM 55-10-01 REPAIR 11 PG. 201 REF. MCO FLEET CYCLE LOG PAGE 9704427 THRESHOLD OF 56,000 TOTAL CYSDR CALA2019092301627Slide · looseON CLOSING OF DOOR 1L. SLIDE CAME LOOSE. LOCK FOR SLIDE REPLACEMENT TECH REPLACED SLIDE REMOVED AND REPLACED 1L DOOR SLIDE. REF AMM 25-66-01-000-802 & 25-66-01-400-801. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1306728 SN OFF 1237 SLIDE, B737NG, OFF 29-2566-9SDR CALA2019062401061Coupler · inoperativeHF RADIOS WOULD NOT TRANSMIT. RESET CB HF1 HF2 STILL INOPERATIVE. REMOVED AND REPLACED LEFT AND RIGHT HF COUPLERS IAW AMM 23-11-61 -400-801 UPTO STEP H.12, INSTALLATION TESTED IAW 23-11-61-400-801. HF1 AND HF2 SYSTEMS OPS CHECKED NORMAL.SDR CALA2017111904145Slide · dislodgedR1 DOOR SLIDE OUT OF THE CONTAINER. SLIDE NOT INFLATED. REMOVED AND REPLACED THE DOOR SLIDE IAW AMM 25-61-01, PAGEBLOCK 401 .SDR CALA2017062601998Battery Pack · dischargedEMERGENCY LIGHTING INOP FROM SEAT ROW 11ABC TO AFT-MOST CABIN. BULLNOSE EMERGENCY LIGHTING ALSO INOP 11ABC TO ROW 22ABC. EMERGENCY LIGHTING OPS CKS OK FROM ROW 11ABC-LAST ROW AND BULL NOSE LIGHTING OPS CKS OK FROM 11ABC-22 ABC. FOUND EMERGENCY LIGHTS INOP AT SDR CALA2017022400446Skin · damaged20 IN CREASE ON RT SIDE OF AIRCRAFT 2.5FT BELOW WING ILLUMINATION LIGHT AND 3FT AFT OF FWD CARGO DOOR. DEPTH AT DEEPEST POINT IS .050 REPAIRED PER ECRA 5330-05961 ACCOMPLISHED RII ON DOUBLER REPAIRED REF SRM 53-00-01 REPAIR 36 ON ECRA 5330-05961.SDR CALA2016100300717Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN AT STA.110 HAS THREE CRACKS MARKED AT 29"1/2"LONG,20"1/2"LONG,AND 11"1"LONG, ALL FROM AFT SPAR. INSTALLED DOUBLER AND FILLER ISSUED DIP TO INSPECTION THRESHOLD 56,000 FLT CYCLES AND REPEATED INSPECTION ON EVERY 9,000 FLT CYCLESSDR CALA2016100300716Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN AT STA 166.30 HAS ONE CRACK 9 1/2" FROM AFT SPAR APPROXIMATELY 1/2" LONG MARKED. INSTALLED DOUBLER AND FILLER ISSUED DIP TO INSPECTION THRESHOLD 56,000 FLT CYCLES AND REPEATED INSPECTION ON EVERY 9,000 FLT CYCLES IAW SRM 55-10-SDR CALA2016070500402Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 402 AND STA 408 BETWEEN STR 26-27 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR IN REF TO ECRA 5331-02113. INTIATED 53-DIP CONTROL 99370 TO ACCOMPLISH REPAIR ON/OR BEFORE JULY 1, 2017 IAW PART 3 OF ECRA 5331-021SDR CALA2016070100397Skin · damagedLIGHTENING STRIKE ON SKIN AT BS 429 AT S26R. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW ECRA 5331-02112.SDR CALA2014102101367Unknown · malfunctionedFOR SDR REPORTING POWER DOWN ACFT FOUND EMER LIGHTS REMAINING ON WITH EMER SWITCH IN THE OFF POSITION. IAW GMM 04-02-16 PG 5 ITEM 17 REF NON-ROUTINE 4352043 CORRECTIVE ACTION. EMER LIGHTS SYS OPERATIONS CHECK IAW AMM 33-51-00-720-801. SYS TESTED GOOD.SDR CALA2014040100408Frame · crackedMAIN CABIN FRAME AFT FACE AT BS 400 BETWEEN STRINGERS 8 & 9L IS CRACKED. REPAIRED IAW SR3-2703967022 & SRM53-00-07 REPAIR 1 FIG 201 & ECRA 5311-01675.SDR CALA2014040100409Battery Pack · dischargedLT & RT OVERWING EMERGENCY EXIT SIGNS & SEAT ROWS 20, 21 & 22 EMERGENCY EXIT LIGHTS INOPERATIVE. TROUBLESHOT AND FOUND EMERGENCY BATTERIES AT POWER SUPPLIES M1694 & M1695 DISCHARGED. R & R BATTERIES IAW AMM 33-51-06 & WDM 33-51-21, OPS CHECKED GOOD.SDR CALA2014040100407Frame · crackedCRACK FOUND ON FRAME DURING NDT HFEC INSPECTION AT BS 440 STRINGER 8 - 9R. REPAIRED FRAME IAW EA5310-04716 REV F FIG 3.SDR CALA2014032400387Skin · crackedRIGHT LOWER HORIZONAL STAB SKIN IS CRACKED AT RIB 157.90 APPROXIMATELY 16 INCHES FROM REAR SPAR. INSTALLED REPAIR IAW SRM 55-10-01 REPAIR 11 FIG 204.SDR CALA2014032400388Skin · crackedRT LOWER STAB SKIN IS CRACKED AT RIB 92.70 APPROXIMATELY 12 INCHES FROM REAR SPAR. INSTALLED REPAIR AT CRACKED AREA RT LOWER STAB SKIN RIB 92.70 APPROXIMATELY 12 INCHES FROM REAR SPAR IAW SRM 55-10-01 REPAIR 11 FIG 204.SDR CALA2014031800353Floor Support · gougedMAIN CABIN FLOOR SUPPORT CORD AT RBL 51 & BETWEEN BS 957 & BS 980 HAS FOUR EACH DEEP GOUGES. MEASURED GOUGED AREAS & FOUND MAX MATERIAL LOSS .053 INCHES & TO CLOSE TO THE EXISTING FASTENERS HOLES. ORIGINAL MAT .080 INCHES, FOUND OUT OF LIMITS IAW SRM 53-70-5SDR CALA2012033000219Drive Unit · inoperativeRADAR FAILS CONTINUOUSLY WITH "WXR FAIL"ICON, ON DISPLAY WITH RADAR OFF ON SHORT FINAL APPROACH "PWS FAIL "INTERMITTENT. NOTE RADAR TEST OK EVERYTIME WITH NO FAULTS. REPLACED UNIT DRIVE PEDESTAL AND TRANSCEIVER WX RADAR REF M/M 3 4-43-11-400-802 AND 34-43-11SDR CALA2011052500392Skin · crackedSUPPORT TASK LT HORIZONTAL STAB LOWER SKIN SECTION CRACK FOUND AFTER C-SCAN INSP PER EA 5510-01843 OP1. SIZE OF CRACK APPROX .5 INCH LONG, LOCATED AT STA 138.70 AND 18 INCHES FROM REAR SPAR. REPAIRED LT HORIZONTAL STAB LOWER SKIN SECT AT STA 138.70 AS PER B7SDR CALA2009040700182Floor Panel · damagedCABIN FLOOR PANEL 232SF HAS SEVERAL PUNCTURE SPOTS. FABRICATED CABIN FLOOR PANEL 232SF REF EC/RA 5320-01448. INSTALLATION WILL BE ACCOMPLISHED ON WORK SEQ 431 ZONE 320C CLOSE CABIN CENTER SECTION DRY.SDR CALA2009040700181Trans Panel · corrodedFORWARD CARGO LEFT TRANSITION PANEL FROM STA 500 TO 500E CORRODED. REMOVED DAMAGED SECTION OF TRANSITION PANEL, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED PER SRM 53-00-53, REPAIR 5.SDR CALA2009040700180Trans Panel · corrodedFORWARD CARGO LEFT TRANSITION PANEL FROM STA 500E TO 500I CORRODED. REMOVED DAMAGED SECTION OF TRANSITION PANEL, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED PER SRM 53-00-53, REPAIR 5.
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