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 FDEA200809163907Connector · damagedLT GEAR (RED AND GREEN) INDICATOR LIGHTS ILLUMINATED IN FLIGHT. ON APPROACH WHEN LANDING GEAR LEVER PLACED DOWN, UNSAFE LIGHT REMAIN ON, RAN QRH AND CHECKED MANUAL MAIN GEAR EXTENSION DOWNLOCKS. FOUND PIN 31 IN PLUG D4658P PUSHED BACK AND LOCK BROKEN. REPLSDR 08FDEA03907Connector · damagedLEFT GEAR (RED AND GREEN) INDICATOR LIGHTS ILLUMINATED IN FLIGHT. ON APPROACH WHEN LANDING GEAR LEVER PLACED DOWN, UNSAFE LIGHT REMAIN ON. RAN QRH AND CHECKED MANUAL MAIN GEAR EXTENSION DOWNLOCKS. FOUND PIN 31 IN CONNECTOR D4658P PUSHED BACK AND LOCK BROKENSDR 08FDEA03773Skin · gougedSCIBE MARKS IN FUSELAGE SKIN FROM STA 690 TO 720D STR 19L TO 19R. CUTOUT DAMAGED SKIN DIMS 50 1/4" BY 33 1/4". FABRICATED NEW SKIN SECTION FROM 2024-T3 .063 PO NR 8204312. FABRICATED REPAIR STRAP AND FABRICATED 2 SHIMS. INSTALLED REPAIR PARTS AT BS 690-720SDR 08FDEA03760Skin · gougedC-3 DOOR EXTERIOR SKIN HAS NUMEROUS DENTS AND GOUGES. FABRICATED NEW EXTERIOR SKIN IAW EA NR 7-5230-123319 AND BOEING DWG NR 65-56927 EA 7-5230-123319.SDR 08FDEA03751Rib · crackedRIGHT WING TIP INTERIOR CRACKED WBL 624. REMOVED WING TIP IAW B727 MM 57-20-001-4. REMOVED WING TIP RIB IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW B727 SRM 51-30-5. INSTALLED NEW RIB IAW B727 SRM 51-30-2 AND REINSTALLED WING TIP IAW B727 MM 57-2SDR 08FDEA03749Skin · tornTORN SKIN NR 1 ENGINE INLET COWL 4 O`CLOCK POS INBD SIDE AT COWL ATTACH LIP. CUT OUT DAMAGED AREA DIMS 1 1/2" BY 1" IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 54-30-3 FIG 3A.SDR 08FDEA03748Fitting · damagedDAMAGED TENSION TIE AT STA 362 STR 17L. REMOVED AND REPLACED DAMAGED TENSION TIE AT BS 362 STR 17L WITH NEW TIE PART NUMBER 65-20984-2 PO NR.SDR 08FDEA03744Skin · damagedOPEN HOLE IN SKIN AT BS 680 STR 23L. FABRICATED AND INSTALLED FREEZE PLUG IAW B727 SRM 51-10-7, FABRICATED RETAINING PLATES USING 7075-T6 .040 PO NR 9007294 DIMS 3" BY 1" AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5330-117034, OPEN HOLE IN SKIN AT BS 680 STR 2SDR 08FDEA03734Skin · dentedSKIN PANEL DENTED STA 615 ON MAIN CARGO DOOR DOUBLER AND TRIPLER AT STR 24L TO 28L. REWORKED SKIN TO ORIGINAL CONTOUR AT BS 620 STR 24L TO 28L IAW FEDEX EA 7-5330-117028, FUSELAGE SKIN PANEL DENT AT STA 615 STR 24L TO 28L REPAIR. INSTALLED DENT DOT IAW FEDEXSDR 08FDEA03720Skin · damagedSCRIBE MARKS IN FUSELAGE SKIN BS 720 6 INCH BETWEEN STR 23LT AND 24 LT. FOUND AREA OUT OF LIMITS IAW SRM 53-30-01 FIG 1. CUT OUT DAMAGED AREA DIMS 2 1/2 INCH BY 1 5/8 INCH IAW SRM 51-10-01 AND 53-30-03 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-03 FIG 2SDR 08FDEA03719Skin · damagedSCRIBE MARKS IN FUSELAGE SKIN BS 720 6 INCHES BETWEEN STR 23 RT AND 24 RT. FOUND AREA OUT OF LIMITS IAW SRM 53-30-01 FIG 1. CUT OUT DAMAGED AREA DIMS 3 INCH BY 2 INCH IAW SRM 51-6-01 AND 53-30-03 FIG 1. FABRICATED DOUBLER IAW SRM 53-30-03 FIG 2. FABRICATEDSDR 08FDEA03643Support · crackedLEFT LOWER TORQUE BOX, UPPER WEB SUPPORT HAS CRACK AT RIVET, STA 1253. CUT OUT AREA FOR ACCESS TO REMOVE SUPPORT ANGLE IAW SRM 51-40-2 & 51-10-1. REMOVED SUPPORT ANGLE IAW SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE IAW DRAWING 65-17518. ALODINED AND PRIMED ANGSDR 08FDEA03620Skin · dentedDENT LT AFT FUSELAGE STA 1070 S18-20L. EVALUATED DENT AT STA 1070 STR 18L TO 20L AND FOUND WITHIN LIMITS IAW SRM 53-30-01 FIG1 BUT DENT CROSSES OVER STR 19L EA 7-5330-117024 "SKIN PANEL DENT AT STA 1074 S18-20L" ISSUED TO ADDRESS DENT CROSSING S19L. PER EA 7SDR 08FDEA03633Actuator · failedNR 8 SLAT FAILED TO RETRACT NORMALLY. LED AMBER ON FRONT PANEL AND S/O PANEL. REMOVED PANELS ON EACH SIDE OF ACTUATOR. FOUND WIRING CLAMPS LOOSE TIGHTENED. WILL CHANGE ACTUATOR OR SWITCH FOR MOCC. REPLACED NR 8 SLAT ACTUATOR REF MM 27-81-032-4. OPS AND LSDR 08FDEA03606Skin · damagedEXTERIOR SKIN OIL CANNED, BL0 STA 640-660. FABRICATED DOUBLER REPAIR FROM 2024T3 .050 PO NR 9007500 DIMS 10" BY 11 1/4 INCH IAW B727 SRM 53-30-3 FIG 1 AND INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 1 AND 51-30-2.SDR 08FDEA03577Spar · corrodedCORROSION ON RIGHT WING FRONT LOWER SPAR CHORD AT FSS 514. REMOVED CORROSION, VERIFIED REMAINING MATERIAL TO BE 0.123", HFEC INSPECTED ALL OPEN HOLES WITH NO DEFECTS NOTED, PERFORMED ULTRASONIC INSPECTION OF BLENDED AREAS, NO DEFECTS NOTED, SPOT FACED FASTENESDR 08FDEA03562Roller Cam · brokenAFTER TAKEOFF CREW REPORTS 2 LOUD BANGS OR POPS. NO ENG INDICATION FLUCTUATIONS OR PRESSURIZATION CHANGES. CREW REPORTS ENTRY DOOR WAS HARD TO CLOSE, BUT NO LIGHTS EVER CAME ON. OCCURED APPROXIMATELY AROUND 14,000 FT. INSPECT CABIN ENTRY DOOR AND FOUND TSDR 08FDEA03544Skin · corrodedEXTERIOR SKIN PILLOWING AND BULGED WITH BROKEN AND PULLED RIVETS STA 309 TO 312 STR 24L. FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO NR 9007561 DIMS 12 INCH BY 7 INCH. FABRICATED STRUCTURAL FILLER FROM 2024-T3 .063 PO NR 9007007 DIMS 12 INCH BY 5 INCH ANDSDR 08FDEA03525Skin · dentedSKIN DENTED RIGHT AFT FUSELAGE FROM C-3 DOOR CUTOUT STA 1148 TO STA 1183 STR 20R. CUT OUT DAMAGED SKIN, FABRICATED REPAIR FILLER USING 2024-T3 .100 PO NR 8221343 DIMS 42 7/8 INCH BY 12 INCH, DOUBLER, TRIPLER. INSTALLED REPAIR PARTS IAW EA 7-5330-117015 - FSDR 08FDEA03524Web · crackedRT LOWER TORQUE BOX INBD WEB HAS A CRACK AT BOLT STA 1223. STOPPED DRILLED CRACK 2 EACH DIMS .250 IAW SRM 51-10-1, HFEC CRACK TO VERFY TERMINATION AT STOP DRILL IAW NDTM PT6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. SDR 08FDEA03523Web · crackedRIGHT LOWER TORQUE BOX INBD WEB IS CRACKED WITH A STOP DRILL AT LIGHTNING HOLE BS 1223. HFEC CRACK TO VERIFY TERMINATION IAW NDTM PT6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-SDR 08FDEA03521Web · damagedAFT AIRSTAIR, LEFT LOWER TORQUE BOX WEB HAS DAMAGED AREA ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, TRIMMED OUT AREA DIMS 1 1/4 INCH BY 3/4 INCH IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLSDR 08FDEA03503Web · crackedLEFT LOWER TORQUE BOX INBD WEB LIGHTNING HOLE ROUTE OUT IS GREATER THAN SRM LIMIT. CRACK DISCOVERED ADJACENT TO ROUTE OUT. STOP DRILLED CRACK IAW SRM 51-10-1. HFEC CRACK INDICATES CRACK ENDS AT STOP DRILL IAW NDTM 51-00-00 FIG 23. FABRICATED 1 REPAIR TO COSDR 08FDEA03502Floorbeam · corrodedMAIN CABIN BS 1070 LBL8 LOWER FLANGE ON FLOORBEAM HAS CORROSION. REMOVED 2 EACH PREVIOUS REPAIRS ON FLOORBEAM IAW SRM 51-30-2. REMOVED CORROSION ON LBL 8, FOUND AREA OUT OF LIMITS IAW SRM 51-10-6 AND 53-10-1. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABSDR 08FDEA03501Seat Track · corrodedMAIN CABIN SEAT TRACK BS 520 BL0 HAS CORROSION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK SECTION USING PREVIOUS GOOD SPLICES IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7.SDR 08FDEA03500Stringer Clip · damagedSTA 355 STR 7R STRINGER CLIP DAMAGED. FABRICATED NEW STRINGER, 2 NEW ANGLES AND NEW EXTRUSION IAW SRM 53-10-3 FIG 2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 2 AND SRM 53-10-2 FIG 9.SDR 08FDEA03499Seat Track · damagedHOLE WITH ZERO EDGE DISTANCE DRILLED IN SEAT TRACK FLANGE STA 990 RBL45. FABRICATED NEW SEAT TRACK SECTIONS. FABRICATED REPAIR ANGLE SPLICES 4 EACH AND INSTALLED NEW SEAT TRACK SECTIONS AT BS 950-1020 RBL 45 IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7.SDR 08FDEA03481Skin · damagedINTERNAL FUSELAGE SKIN AT BS 355 BELOW STRINGER 7RT HAS A DRILL START. DRILLED A .161 DIA HOLE AND INSTALLED A NAS1097AD5 RIVET IAW EA NR 7-5330-117006 AND SRM 51-30-2.SDR 08FDEA03443Floorbeam · corrodedMAIN CABIN BS 1110 LBL 65 AND LBL 45 FLOORBEAM UPPER FLANGE HAS CORROSION. REPAIRED MAIN CABIN FLOORBEAM UPPER FLANGE BS 1110 LBL 57 CUTOUT AREA DIMS 3 1/2 INCH BY 1 INCH, FABRICATED REPAIR ANGLES (2EA). FABRICATED FILLER. INSTALLED REPAIR PARTS AT BS 1110 SDR 08FDEA03431Skin · crackedLARGE HOLE IN RT ELEVATOR, INSIDE NR 3 BALANCE PANEL ACCESS, PUNCTURE HOLE. REMOVED WEB AND ANGLE IAW SRM 51-30-2. FABRICATED WEB AND (1) EA ANGLE IAW DRAWING 65-26163 REV C. BONDED WEB PER BMS 5-69 IAW DRAWING 65-26163 REV C. HEAT TREATED ANGLE IAW ER 2-3SDR 08FDEA03399Handle · gougedLEFT AND RIGHT MLG DOOR RELEASE HANDLES ARE GOUGED. BLENDED GOUGES AT LEFT AND RIGHT MLG DOOR RELEASE HANDLES IAW EA 7-3210-117011.SDR 08FDEA03396Lap Joint · gougedSKIN GOUGED RIGHT FUSELAGE LAP SEAM FWD OF STA 720E AT STR 19R. CUTOUT DAMAGED AREA DIMS 3 INCH BY 4 1/2 INCH IAW SRM 53-30-3. FABRICATED DOUBLER, FABRICATED REPAIR FILLER IAW SRM 53-30-3 FIG 14. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED RSDR 08FDEA03393Fitting · crackedLT WING, EVALUATE PREVIOUS REPAIR AT INBD LOWER CORNER OF NR 7 SPOILER FITTING AT FALSE SPAR. REMOVED IMPROPER REPAIR IAW SRM 51-30-2 AND FEDEX DRAWING SR-27-57-038 REV C. REMOVED NR 7 SPOILER FITTING AND DOUBLER, TRIMMED OUT WEB, FABRICATED NEW DOUBLER USISDR 08FDEA03394Seat Track · corrodedCORROSION ON SEAT TRACK FLANGES AND ATTACHING HARDWARE, STA 1010 10 INCH TO STA 1050, LBL 45 FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED (3) EA SECTIONS OF SEAT TRACK FROM BS 1010 TO 1130 IAW B727 SRM 51-30-2. FABRICATED NEW SECTION OF SEAT TSDR 08FDEA03361Keelbeam · crackedLEFT KEEL BEAM CHORD IS CRACKED AT STA 880. REMOVED AND DISCARDED EXISTING GUSSET PLATE AND FASTENERS COMMON TO THE KEEL BEAM CHORD IAW FEDEX EA 7-5310-117026. VERIFIED END OF CRACK USING HFEC IAW B727 NDTM 51-00-00 FIG 1. TRIMMED UPPER FLANGE OF KEEL BEAM SDR 08FDEA03360Keelbeam · crackedRIGHT KEEL BEAM CHORD IS CRACKED AT STA 872. ACCOMPLISHED REPAIR ON RIGHT KEEL BEAM CHORD AT STA 872 IAW FEDEX EZ 7-5310-117026, MLG WHEEL WELL KEEL BEAM CRACK AT BS 872 REPAIR.SDR 08FDEA03359Splice · gougedSKIN GOUGED LEFT FUSELAGE LAP SEAM FWD OF 720E AT STR 19L. FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO NR 9006288 DIMS 14 INCH BY 7 1/2 INCH. FABRICATED STRUCTURAL FILLER FROM 2024-T3 .063 PO NR 9006773 DIMS 14 INCH BY 5 INCH. INSTALLED REPAIR PARTS AT FSDR 08FDEA03358Frame · chafedFRAME DAMAGED STA 360 STR 2R. CUTOUT DAMAGED AREA DIMS 1 1/8 INCH BY 1 INCH, FABRICATED REPAIR ANGLE FROM 7075-0 .063 PO NR 9007470 DIMS 9 INCH BY 3 INCH BY 1 INCH. INSTALLED REPAIR ANGLE AT BS 360 STR 2R IAW B727 SRM 53-10-4 FIG 2 AND SRM 53-10-2 FIG 3.SDR 08FDEA03357Seat Track · corrodedCORROSION AT SEAT TRACK OUTBOARD FLANGE TOP STA 425 RBL 45. FABRICATED NEW SEAT TRACK SECTION FROM BS 390 TO BS 480. FABRICATED REPAIR SPLICES. INSTALLED NEW SEAT TRACK SECTION AND SPLICE AT BS 390 TO BS 480 RBL 45 IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG SDR 08FDEA03356Floorbeam · corrodedSURFACE CORROSION STA 720D RBL 12 TOP OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 4, CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3, FABRICATED UPPER CHORD, 2 SUPPORT ANGLES AND 2 REINFORCEMENT STRAPS IAW SRM SDR 08FDEA03352Skin · dentedFUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19-20L. EVALUATED 02 DENTS BELOW L1 DOOR USING MECHANICAL MEANS AND FOUND DENTS WITHIN LIMITS, BUT DENTS ARE LESS THAN 10 INCHES FROM THE LAP SEAM IAW SRM 53-30-1 FIGSDR 08FDEA03351Skin · dentedFUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19 - 20L. EVALUATED 2 DENTS BELOW L1 DOOR USING MECHANICAL MEANS DENT NR 1 A: 1.9 Y: .031 A/Y: 61.2 AND DENT NR 2 A: 1.2 Y: .007 A/Y: 171.4. A/Y MEASUREMENTS ARE WISDR 08FDEA03350Skin · dentedFUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 VERTICAL DENTS AT STA 320 BETWEEN STR 17L - 19L. EVALUATED 2 DENTS AND MEASURED DENTS A: 1.0 Y: .019 A/Y 45.2 AND DENT 4 A: 2.4 Y: .053 A/Y 45.2, A/Y RATIO WITHIN LIMITS BUT DENTS ARE COMMON TO TEAR STRAP AND LESS SDR 08FDEA03315Skin · damagedNR 1 ENGINE NOSE COWL SKIN DAMAGED AT 9 O'CLOCK POSITION CUT OUT DAMAGE AREA DIM 4 3/4 BY 3 1/2 IAW B727 SRM 54-30-3 FIG 5. CUT OUT ACCESS HOLE DIM 5 IN ABOVE DAMAGE IAW B727 SRM 54-30-3 FIG 3. FABRICATED DOUBLER REPAIRS FROM 2024T3, 0.040 INCH AND FILLER FRSDR 08FDEA03314Support Beam · crackedLT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 7 IS CRACKED AT WBL 122 REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM FROM BAC 1506 860 7075 T6 (DIM 81 INCHES IN LENGTH) AND TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED "J" BEASDR 08FDEA03313Support Beam · crackedRT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 8 IS CRACKED AT WBL 123 REMOVED "J" BEAM IAW B727 SRM 51-30-2 AND FABRICATED NEW "J" BEAM FROM BAC1506-860 7075-T6. APPROX DIM 81 INCHES IN LENGTH IAW B727 SRM 51-30-5 AND SRM 57-20-2 FIG 2. TREATED ANSDR 08FDEA03256Connector · damagedDURING CRUISE AT FL 350 THE RUDDER LOAD LIMITER LIGHT AND BOTH THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED AT THE SAME TIME. DURING THE DESCENT THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED INTERMITTENTLY WHILE THE RUDDER LOAD LIMITER REMAINED ILLUMINATSDR 08FDEA03192Skin · damagedEXISTING TOOL MARKS ON SKIN AT FUSELAGE STA 334 BY UNDER HAT SECTION AREA OF STR 10R. BLENDED OUT DAMAGE IAW SRM 51-10-1, AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2. REPAIRED SKIN IAW EA 7-5330-122358-FUSELAGE, AD 2002-07-09 AND AD 98-11-03-65-18420SDR 08FDEA03164Frame · dentedFRAME AT STA 344 DENTED AT STR 5L AT 9G BULKHEAD. CUT OUT DAMAGE FROM FRAME IAW SRM 53-10-4 FIG 2. FABRICATED NEW FRAME REPAIR AND REPAIR FILLER IAW SRM 53-10-4 FIG 2 AND 53-10-2 FIG 3 AND 51-20-1. HEAT TREATED FRAME REPAIR IAW FAS ENGINEERING REPORT 2-3715SDR 08FDEA03161Skin · gougedT/E OF LT OB FOREFLAP HAS (2) EA DEEP GOUGES ON UPPER SURFACE. REMOVED DAMAGED AREA IAW SRM 51-40-20 PAGE 12. FABRICATED FILLER AND DOUBLER IAW SRM 51-40-20 PAGE 59. HOT BONDED FILLER AND DOUBLER ON SEALED EDGES AND PRIMED AREA IAW SRM 51-40-20 PARAGRAPH 7-
Back to Boeing 727-233