Boeing 727-233
Service difficulty reports · 3,034
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '727233' 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 aircraft_model_key = '727233' 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 FDEA200911133948Actuator · leakingCOMPLETE LOSS OF SYS A HYDRAULICS DURING FLAP RETRACTION. FOUND ACTUATOR ABOVE TAIL SKID LEAKING OUT OF THE HSG. ORDERING NEW ACTUATOR. R&R TAIL SKID ACTUATOR PER MM 32-71-012-4 AND HAD TO ADJUST ACTUATOR PER MM 32-71- 001-5 LEAK AND OPS CKS GOOD. RAN NR 1SDR FDEA200911093923Shear Tie · corrodedINT FUSELAGE BS 303.9 BETWEEN STR 22R-23R SHEAR TIE HAS CORROSION. CUT-OUT DAMAGED AREA APPROX DIM OF CUT-OUT 2" X 5" IAW SRM 53-10-4. FABRICATED SHEAR TIE REPAIR FROM PN 7075T6 .050 PO NR 9008963 APPROX DIM: 4" X 5 1/2" IAW SRM 53-10-4 FIG H, 53-10-2 AND 5SDR FDEA200911083920Skin · misrepairedDOUBLER EXT SKIN BS 440 STR 25L NO EDGE DISTANCE BETWEEN FASTENERS. CUT-OUT DAMAGED AREA UPPER & LWR SKIN, FABRICATED REPAIR DOUBLER, TRIPLER, REPAIR FILLER, BEAR STRAP FILLER, UPPER FILLER, DOUBLER FILLER AND TAPERED FILLER, MILLED BEAR STRAP FILLER, FABRISDR FDEA200911073886Skin · damagedRT FWD OVERWING EMER EXIT HATCH EXTERIOR SKIN HAS SEVERAL AREAS OF SKIN EDGE DAMAGE. REMOVED ACCESS PANEL AND REMOVED COVER SUPPORT IAW SRM 51-30-2. CUT-OUT DAMAGE AREA DIM: 3 1/2" X 4 1/8" IAW SRM 52-00-3 FIG 3, REV 101. FABRICATED REPAIR DOUBLER IAW SRM 5SDR FDEA200911053853Relay · false activationAFTER DEPARTING EWR AND CLIMBING THROUGH 16000 FT MAIN CARGO DOOR "B" LIGHT ILLUMINATED. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. RELEASED FOR SERVICE IAW MEL: 52-15-01. REMOVED AND REPLACED CARGO DOOR WARNING SYS "B". RELAY R9107. OPS CHECKS NORMAL ISDR FDEA200910303747Stringer · corrodedINT FUSELAGE BS 312-300 STR 25 RT HAS CORROSION IN CHANNEL. CUT OUT DAMAGED STRINGER APPROX DIM 18" LONG IAW SRM 51-30-2, FABRICATED NEW STRINGER FILLER FROM BAC1498-139 PO#29111206 APPROX DIM 20 5/8" FABRICATED 2 ANGLES, FABRICATED CHANNEL, AND FABRICATED SDR FDEA200910303746Stringer · corrodedINT FUSELAGE BS 300-312 STR 24 RT IS CORRODED IN CHANNEL. REMOVED CORRODED SECTION OF STRINGER 15.6 " LONG IAW SRM REV 101 51-10-1. FABRICATED STRINGER FILLER, 4 ANGLES, 2 CHANNELS, & STRAPS, IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED REPAIR PARTS ISDR FDEA200910303745Skin · damagedMAIN CARGO AREA, BS 450, STR 3L, NO EDGE DISTANCE BETWEEN FASTENERS. REMOVED FASTENERS AREA IAW SRM 51-30-2, CUT OUT DAMAGE STRINGER AREA IAW SRM 53-10-3 FIG 3, FABRICATED FILLER. FABRICATED PLATE NR 1. FABRICATED PLATES NR 2 IAW SRM 53-10-3 FIG 3 53-10-2 SDR FDEA200910303744Skin · corrodedAFT CARGO COMPARTMENT BS1010 OTBD OF STR 29L LEVELING COMPOUND MISSING AND CORROSION ON SKIN. CUT OUT DAMAGE SECTION IAW SRM 53-10-3 FIG 3A. FABRICATED DOUBLER AND 1EA FILLER IAW SRM 53-30-3 FIG 3A. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS DSDR FDEA200910283718Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS360 - BS420, LBL 24. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 344-480 LBL 24, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 PO NR 9006020 APPROX LENGTH 136" AND INSTALLED NEW SEAT TRACK SECTION USING PREVIOUS GOOD CONDITSDR FDEA200910273852Skin · damagedDOUBLER EXT SKIN BS 460 STR 27L, NO EDGE DISTANCE BETWEEN FASTENERS. CUT OUT DAMAGE ON LOWER FLANGE OF STRINGER 27L, 3/4" X 3/4" IAW SRM 51- 10-1 REV 101, FABRICATED FILLER FROM BAC1514-1559, AND DOUBLER FROM BAC1509-100146 6 1/2" LONG IAW SRM 51-40-3. ISDR FDEA200910273692Angle · crackedRT W/W VERTICAL ANGLE IS CRACKED AT BS 870, RBL 8. REMOVED CRACKED ANGLE IAW SRM 51-30-2 REV 101. LOCATED DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 51-30-2.SDR FDEA200910273740Angle · crackedLT WING STR CRACKED AT STR TO RIB ATTACH POINT WS 686.5 STR 10 STOP DRILLED CRACK .190 DIA, HFEC INSPECTED STOP DRILL AREA NO DEFECTS NOTED, FABRICATED ANGLES REPAIR. FABRICATED RADIUS FILLER AND INSTALLED REPAIR PARTS AT LT WING STR 10 WS 686.5 IAW EO 7- 5SDR FDEA200910273695Skin · dentedDENT IN NR3 ENGINE NOSE COWL LWR SKIN AT NAC STA 69.00. CUT OUT DAMAGE 3 3/8 X 5 7/8 IAW SRM REV 101, 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024T3, .050 X 7 1/2 X 9 3/8, PO NR 9008452 AND FILLER FROM 2024T3 .040 X 5 7/8 X 3 3/8", PO NR 9008875 IAW SRM 54-SDR FDEA200910273691Frame · corrodedAFT CARGO COMP BS 1130 OB OF STR 29LT. AFT FRAME FLANGE HAS CORROSION. REMOVED AFT FLANGE ANGLE AT BS 1130 OTBD OF STR 29L IAW SRM REV 101 51-30-2. FABRICATED REPLACEMENT ANGLE FROM 7075T6 .063 X 2 1/8" X 6 1/2", PO NR 9008729 IAW SRM 51-20-1, FIG 7 AND 53-SDR FDEA200910213651Angle · crackedLEFT I/B MID FLAP CRACKED AT CUT-OUT IN T/E ANGLE. REMOVED CRACKED SECTION OF LT IB MID FLAP TE ANGLE 46" LONG IAW SRM REV 101, 51-30-2. LOCATED, DRILLED AND DEBURRED NEW SECTION OF TE CHORD IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 51-30-2.SDR FDEA200910213637Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 BL 0. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 344-480 BL0 , FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 PO 9006020 APPROX DIM 136" & INSTALLED NEW SEAT TRACK USING EXISTING GOOD SPLICE IAW SRM 53-10-5 FIGSDR FDEA200910213641Torque Box · crackedAFT AIRSTAIRS, RT LR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT BS 1223. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIR RT LWER TORQUE BOX LOWER LIGHTNING HOLE AT BS 1213 IAW SRM REV 101 51-10-1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTASDR FDEA200910213640Torque Box · crackedAFT AIRSTAIRS, RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT BOTTOM AT BS 1213. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIRS RT LOWER TORQUE BOX LOWER LIGHTNING HOLE AT BOTTOM BS 1213 IAW B727 SRM REV 101 51-10-1. FABRICATED DOUBLER FROM 7075T6 .032SDR FDEA200910213639Torque Box · crackedAFT AIR STAIRS, RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT TOP AT BS 1213. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIRS RT LOWER TORQUE BOX LOWER LIGHTNING HOLE AT BS 1213 IAW B727 SRM REV 101 51-10-1. FABRICATED DOULBER FROM 7075T6 .032" X 4" X 2 SDR FDEA200910213622Frame · damagedSTA 303.9 FRAME, WEB CUTOUT AT STR 15L AND STR 16L HAVE SHARP RADIUS. ACCOMPLISHED REPAIR IAW EA NR 7-5310-135505.SDR FDEA200910203736Skin · damagedTRIPLER EXT SKIN BS 620 STR 25L TWO DRILL STARTS. REMOVED FASTENERS AT EXT SKIN BS 620 STR 25L IAW SRM 51-30-2, CUT OUT DAMAGED AREA APPROX 1.05" X 4.6" IAW SRM 53-30-3 FIG 1A. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-30SDR FDEA200910203735Angle · crackedRT INBD MID FLAP FWD LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW PULLEY MECHANISM WBL112. REMOVED ACCESS PANEL IAW SRM 51-30-2 AND REMOVED DAMAGED ANGLE IAW SRM 51-40-4. FABRICATED REPAIR ANGLE IAW SRM 51-40-4 TREATED & PRIMED ANGLE IAW B727 SRM 51-10-2. INSDR FDEA200910203650Skin · damagedTRIPLER EXTERIOR SKIN BS 480 STR 25L HAS TWO DRILL STARTS CUT OUT DAMAGE 3 1/4 SQ IAW SRM REV H 53-30-3 FIG 1A. FABRICATED REPAIR DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG 1A. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1A.SDR FDEA200910203653Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 RBL 24. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1, SRM 51- 30-2, AND SRM 53-10-1 FIG 3A.SDR FDEA200910203655Skin · damagedMAIN CARGO AREA BS 640 STR 3L & STR 4L, NO EDGE DISTANCE. CUT OUT DAMAGED AREA OF SKIN IAW SRM 53-30-3, CUT OUT DAMAGED AREA OF TEAR STRAP IAW SRM 53-30-4 FIG 9. FABRICATED TEAR STRAP REPAIR IAW SRM 53-30-4 & 51-30-5, FABRICATED EXTERNAL REPAIR DOUBLER. FASDR FDEA200910203654Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 LBL 24.SDR FDEA200910203652Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 BL0.SDR FDEA200910203636Skin · gougedRT WING INBD FORE FLAP OUTBD LEADING EDGE IS GOUGED AT WBL 482. BLENDED GOUGE ON RT WING INBD FORE FLAP LE SKIN AT O/B END IAW FEDEX B727 SRM REV 101, 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024T3 .063 X 4 5/8" X 3 7/8" PO#9008729 IAW B727 SRM 57-50-4. INSDR FDEA200910183605Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED AT BS 1243 - MARKED. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 INSTALLED REPAIR DOUBLER IN AFT AIRSTAIR RT LOWER TORQUSDR FDEA200910183600Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED BS 1223 - MARKED. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 INSTALLED REPAIR DOUBLER IN AFT AIRSTAIR RT TORQUE BOX LIGHSDR FDEA200910183604Torque Box · crackedAFT AIRSTAIR AREA - RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED BS 1223. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER ON RT LOWER TORQUE BOX IAW SRM 51-30-2 REV 101.SDR FDEA200910183603Angle · crackedRT WING OTBD MID-FLAP UPPER CHORD ANGLE IS CRACKED ABOVE INBD PULLEY AT WBL 320. REMOVED AND REPLACED RT OTBD MID FLAP ASSY IAW MM 27-51-011-4. ADJUSTED/OPS CHECK GOOD IAW MM 27-51-000-5.SDR FDEA200910153587Angle · damagedPLUG FOUND NEXT TO FASTENER BS 1183 CHORD ANGLE AFT PIT BETWEEN STR 28L TO STR 29L. TRIMMED OUT BS. 1183 BULKHEAD WEB APPROX DIM: 30 1/2" X 9 1/4", BULKHEAD BEAM CUT-OUT DIM: 33 5/8". FABRICATED BULKHEAD WEB REPAIR DOULBER, & FILLER. FABRICATED BEAM REPAIRSDR FDEA200910153578Vertical Beam · misinstalledFASTENERS HAVE NO SPACING AFT PIT BS 1183 LBL 17.8 VERTICAL BEAM. TRIMMED OUT BS 1183 BULKHEAD WEB APPROX DIM: 30 1/2" X 9 1/4", BULKHEAD BEAM CUT-OUT DIM: 33 5/8". FABRICATED BULKHEAD WEB REPAIR DOUBLERS, FILLER. FABRICATED BEAM REPAIR TEE REPAIR ANGLES, FSDR FDEA200910143601Angle · crackedNR 8 SLAT LWR AFT CHORD ANGLE IS CRACKED AT INBD UP STOP PAD. FABRICATED ANGLE REPAIR FROM EXTRUSION BAC 1514-1559 2024T3-511, PO NR 29111160, DIM: 11" AND OTHER 6" (2 ANGLES) IAW SRM 51-40-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR ANGLESSDR FDEA200910143556Line · leakingAPPROX T/O 40 MINS S/O NOTICED HYD SYS A QTY NEAR 0. SHORTLY AFTER THAT THE SYS "A" PRESSURE STARTED TO FLUXUATE DRYING, RAN OF THE QRH CHECKLIST. SYS A HYD FLUID SHUT OFF SWITCHES WERE BOTH TURNED OFF FOR THE ENGINES NR 1 AND NR 2 AT 13/0145Z. (OFF FOR 1 2SDR FDEA200910053479Stringer · corrodedCORROSION ON OTBD SIDE OF STR 28L BETWEEN STA 490 AND 500. CUT OUT DAMAGED AREA, FABRICATED 2 REPAIR SPLICES, FABRICATED STRINGER FILLERS AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.SDR FDEA200910053478Skin · corrodedCORROSION ON SKIN AT STA 496 OTBD OF STR 28L. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3, 53-30-2 AND 51-30-2.SDR FDEA200910013455Stiffener · crackedNLG LT TRUNNION FITTING AFT VERTICAL STIFFNER CRACKED. REMOVED VERTICAL STIFFNER IAW SRM 51-30-2. LOCATED AND DRILLED NEW VERTICAL STIFFNER PN 65-19863-5 PO NR 29105141 IAW SRM 51-30-5. INSTALLED NEW VERTICAL STIFFNER IAW SRM 51-30-2.SDR FDEA200909293427Seat Track · corrodedMAIN CABIN SEAT TRACK BS 480 - 380 BL0 IS CORRODED AT I/B FLANGE. FABRICATED NEW SEAT TRACK SECTION FROM BS 380 TO BS 480 BL 0 USING PN BAC 1520-792 PO NR 9006020 APPROX 109.6250 INCH FABRICATED REPAIR SPLICE ANGLES AND REPAIR STRAP IAW SRM 53-10-5 FIG 1, TRESDR FDEA200909283433Support Fitting · missingMAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, LBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.SDR FDEA200909263456Skin · damagedNR 2 ENGINE "S" DUCT INLET NOSE COWL CAP HAS DENT AT 8 O'CLOCK POSITION, BS 1101. EVALUATED DENT AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA , FABRICATED 2 DOUBLERS AND LIP SKIN FILLER, HEAT TREATED PARTS TO T4 CONDITION AND INSTALLED IAW SRM 54-30-1, 54-SDR FDEA200909253388Structure · corrodedNLG WHEEL WELL UPPER STRUCTURE - CORROSION ON MID CHORD UPPER SURFACE AT APPROX STA 350, LT SIDE, ( INSIDE FWD WALKWAY ACCESS). REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 5312412 PO NR 29105100 AND INSTALLED IAWSDR FDEA200909243430Skin · gougedFWD PIT - SKIN GOUGED AT BS 480, AFT SIDE, BETWEEN STRINGERS 27L AND 26L. CUT OUT DAMAGED TEAR STRAP, CUT OUT SKIN, FABRICATED SKIN DOUBLER, TRIPLER, STRUCTURAL FILLER, FILLER, TEAR STRAP REPAIRS AND SHEAR TIE REPAIR, HEAT TREATED PART TO T6 CONDITION IAW SDR CA090928001Wire · broken(CAN) AFTER DEPARTURE FROM YVP, THE FLIGHT CREW ADVISED OF A NOSE LANDING GEAR DISAGREEMENT LIGHT. THE GEAR WAS RECYCLED SEVERAL TIMES AND THE DISAGREEMENT LIGHT REMAINED. MAINTENANCE DISCOVERED A BROKEN WIRE IN THE NOSE LANDING GEAR DOWNLOCK WIRE HARNESS. WISDR FDEA200909233371Seat Track · corrodedCORR AT SEAT TRACK LBL 45, STA 852-STA 870 REMOVED OLD SEAT TRACK ON LBL 45 STA 852 TO STA 870 IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-1466 PO 8205123 DIM: 16 INCHES X 4 INCHES IAW SRM 53-10-2 TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2 SDR FDEA200909233364Motor · leakingLOST SYS A HYD FLUID DURING CLIMBOUT DID QRH CHECKLIST. SECURED SYS A HYD PUMPS AND CLOSED FLUID SHUTOFF SWITCHES IAW QRH. REMOVED AND REPLACED BOTH FLAP MOTORS IAW 27-51-062-4, REMOVED AND REPLACED ENG NR 1 AND 2 CASE DRAIN FILTERS IAW 29-11-041-2, REMOVED SSDR FDEA200909223426Seat Track · corrodedMAIN CABIN SEAT TRACK BS 440-460, LBL 24 IS CORRODED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED ANGLES, ONE STRAP, AND NEW SEAT TRACK SECTION AND INSTALLED PARTS IAW SRM 53-10-5 AND 51-30-2.SDR FDEA200909223367Switch · inoperativeON CLIMBOUT RT INBD LED WOULD NOT RETRACT. RUN QRH, RTB, NO RESTRICTION NR 4 L/E FLAP HAS JUMPER CABLE INSTALLED IAW MM 27-82-000-1. REMOVED AND REPLACED AND CHECKED NR 4 L/E SWITCH IAW AMM 27-82-011-4, ALL SYS CHECKED GOOD AT THIS TIME. PREMATURE REMOVAL/I
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