Boeing 727-22
Service difficulty reports · 1,282
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 = '72722' 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 = '72722' 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 98FDEA00011Chord · corrodedCORROSION (C53-224-03 1, 2) ON RT MID CHORD BS 315 TO 335, RBL 15, WL 169 WILL REQUIRE REMOVAL OF NOSE LANDING GEAR TO GAIN ACCESS. *S/D* REMOVED DAMAGED CHORD AND INSTALLED NEW CHORD BS 259 TO 351, WL 169, RBL 15 IAW FEDEX DRG 65-18415.SDR 98FDEA00010Stringer · corrodedCORROSION ON STR 29 LT KEEL BEAM LT BS 1080, WL 140. *S/D* REMOVED CORROSION ON STR 29L AT BS 1080 TO 1095, WL 140. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED CORRODED PIECE IAW FEDEX SRM 53-10-3. FABRICATED REPAIR PARTS PER FEDEX SRM 53-10-SDR 98FDEA00007Overheat Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT PASSING FL270. ENGINE ANTI-ICE WAS OPEN DURING CLIMBOUT. NR 1 BLEED WAS OPENED AND NR 2 BLEEDS CLOSED AND RED TAB PROCEDURE WERE INITIATED. THE LIGHT EXTINGUISHED SHORTLY AFTER NR 2 ENGINE ANTI-ICE WSDR 97FDEA00893Actuator · loose97-0253 - RIGHT MAIN LANDING GEAR RED DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION. GREEN GEAR LIGHT OUT. RIGHT MAIN GEAR DOOR CAUTION AMBER LIGHT ON SO PANEL WAS ILLUM. CREW FELT THE RIGHT MAIN GEAR DOWN AND LOCKED. WHEN GEAR HANDLE WAS PUT DOWN RIGHT MAISDR DHL97707004Strut · crackedCRACK FOUND ON RIGHT MLG STRUT BARREL APPROX 13 LONG. REMOVED AND REPLACED LANDING GEAR ASSY PER DHL JOB INSTRUCTION CARD.SDR 97FDEA00866Skin · corrodedCORROSION (C53-100-01) ON EXTERIOR SKIN FROM BS 1149 TO BS 1153, RBL 2, WL 148. *S/D* REMOVED SECTION OF SKIN (9.7 X 7.5) AT BS 1149 TO 1159, RBL 2 LBL 2, WL 148, APPLIED SKIN PATCH IAW FDE SRM 53-30-3.SDR 97FDEA00863Skin · dentedDENTED EXTERIOR SKIN AT BS 1135 BETWEEN STRINGERS 18L AND 19L, LBL 65, WL 192. *S/D* ACCESSED DAMAGED AREA AND INSTALLED COUNTERSINK WASHERS, FABRICATED PARTS AND INSTALLED FASTENERS AND ALL ACCESSED PARTS PER FEDEX SRM 53-30-03.SDR 97FDEA00862Frame · crackedBS 500 FRAME IS CRACKED UNDER FLOOR SUPPORT AT RBL 9, WL 156. *S/D* REPAIRED FRAME AT BS 500, RBL 9, WL 156 UNDER FLOOR SUPPORT IAW FEDEX SRM 51-40-3.SDR 97FDEA00857Crease Beam · corrodedNR 0125 003 CORROSION (C53-224-06) ON CREASE BEAM VERTICAL FLANGE BS 310-346, LBL 62, WL 209. REMOVED OLD CORRODED CREASE BEAM AND DRILLED AND INSTALLED FASTENERS IN NEW CREASE BEAM BS 285 - BS 360, LBL 62, WL 208 IAW FEDEX SRM 51-30-2, 53-10-1, 51-30-5.SDR 97FDEA00856Stringer · corrodedWHILE WORKING CUSTOMER CARD NR NR0154, FOUND CORROSION ON STR 30, BS 1148, WL 142. *S/D* REMOVED DAMAGED STRINGER AT BS 1138 TO BS 1158, STR 30, WL 142 AND REPAIRED IAW FED SRM 53-10-3.SDR 97FDEA00851Skin · corrodedCORROSION (C53-100-01) ON EXTERIOR SKIN AT BS 1080 BETWEEN STR 27L AND 28L, WL 144, LBL 12 TO LBL 24. *S/D* REPAIRED SKIN AT BS 1080 BETWEEN STR 27L AND 28L, LBL 12 TO LBL 24 PER FEDEX SRM 53-30-3.SDR 97FDEA00850Frame · crackedBS 680 FRAME HAS CRACK EMANATING FROM RADIUS IN CUTOUT FOR STR 26 RT. *S/D* STOP DRILLED CRACK AT BS 680, STR 26 RT PER FEDEX SRM 51-10-1 AND REPAIRED CRACK PER FEDEX SRM 51-40-3.SDR 97FDEA00849Panel · malfunction97-0237 NOSE GEAR DID NOT INDICATE DOWN SAFE (GREEN LIGHT NOT ON.) NOSE GEAR LIGHT WOULD NOT TEST. GEAR DOOR LIGHT TRANSITIONED NORMALLY WITH EXTENSION AND RETRACTION. RED UNSAFE NOSE LIGHT TRANSITIONED NORMALLY AS WELL. FOUND LANDING GEAR/DOOR ANNUNCIATORSDR 97FDEA00830Connector · contaminatedRIGHT MAIN LANDING GEAR DOOR WILL NOT STAY CLOSED WITH GEAR LEVER IN OFF POSITION. CYCLED GEAR, NO HELP. DRAINED WATER FROM CANNON PLUG AND CLEANED, OPERATIONAL CHECK OF GEAR DOOR GOOD PER MAINTENANCE MANUAL 32-12-1.SDR 97FDEA00829Switch · inoperativeEQUIPMENT ACCESS DOOR LIGHT INOPERATIVE. AIRCRAFT TOOK OFF WITH ELECTRICAL EQUIPMENT COMPARTMENT OPEN. RAMP ACCOMPLISHED PUSH BACK, INSPECTED ELECTRICAL EQUIPMENT BAY. NO DAMAGE NOTED. CLOSED ELECTRICAL EQUIPMENT DOOR. DEFERRED ELECTRICAL EQUIPMENT DOOR WSDR 97FDEA00806Keel Beam · corrodedNR 0388 016 CORROSION ON THE L/H KEEL BEAM BETWEEN SKIN BS 1065. *** S/D *** REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED PORTION BS 1057 TO 1087. REMOVED DAMAGED SKIN BS 1065. REMOVED DAMAGED SHEAR TIE. FABRICATED REPAIR PARTS. INSTSDR 97FDEA00801Shear Tie · corrodedNR 0446 014 CORROSION (C53-113-01(2)) IN THE SHEAR TIE BS 990, BETWEEN STRINGERS 29 & 30 R/H. *** S/D *** REPAIRED SHEAR TIE AT BS 990, RBL 6, WL 151 IAW FED-EX SRM 53-10-4.SDR 97FDEA00800Splice · corrodedNR 0421 015 CORROSION IN THE STRINGER SPLICE AT BS 1057, STR 28 R/H. *** S/D *** REMOVED STRINGER SPLICE AT BS 1057. REMOVED STRINGER END PIECE AT BS 1040-1057. FABRICATED STRINGER END BS 1040-1057 AND INSTALLED WITH STR SPLICE AT BS 1057. IAW FESDR 97FDEA00784Floorbeam · corrodedNR 0253 009 CORROSION (C53-224-06) ON FLOORBEAM BS 344, RBL 15-LBL 60, WL 208. UPPER CHORD OF 344 FLOORBEAM, RBL 65 TO LBL 65, WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED CORRODED UPPER CHORD FROM RBL 65 TO LBL 65 AND INSTALLED NEW UPPER CHORD PER FED-EX DSDR 97FDEA00783Frame · crackedNR 0412 010 AFT CARGO BAY AT BS 1130, STR 26L THE FRAME IS CRACKED IN THE J SECTION. *** S/D ***INSTALLED DOUBLER ON FRAME AT 26L BS 1130 AFT CARGO BAY AS PER FED-EX SRM 51-40-3.SDR 97FDEA00782Rib · corrodedNR 0083 011 NR 2 K-FLAP CORRODED AT I/B BONDING JUMPER TO BULLNOSE. REMOVED CORROSION ON NR 2 K-FLAP I/B BULLNOSE ATTACH (LOWER) POINT FLANGE THICKNESS .140. REMOVED .030 WITHIN LIMTS PER FED-EX DWG NR SR 27-57-010. UPPER ATTACH POINT OUT OF LIMITS. INSTALSDR 97FDEA00781Rib · corrodedNR 0173 012 CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH POINTS ON NR 4 K-FLAP BULLNOSE, O/B END. REMOVED CORROSION AT BONDING WIRE UPPER AND LOWER ATTACH POINTS ON NR 4 K-FLAP BULLNOSE O/B END IAW FED-EX DRWG SR 27-57-010 REV C AND FED-EX SRM 57-50-3. USDR 97FDEA00779Retract Mech · failedDURING INITIAL CLIMB AFTER TAKEOFF, THE RIGHT MLG DOOR LIGHT CAME ON AFTER THE LANDING GEAR WAS UP. THE RIGHT MLG DOOR LIGHT WENT OUT AFTER SEVERAL REPEATED CYCLING ATTEMPTS ON GEAR HANDLE. PERFORMED MLG DOOR WARNING SWITCH ADJUSTMENT/TEST. OPS CHECK NORMALSDR 97FDEA00777Floorbeam · corrodedNR 0103 008 CORROSION (C53-224-06) ON FLOORBEAM BS 328, LBL 37, WL 208. REMOVED CORROSION (C53-224-06) FOUND TO BE OUT OF LIMITS. REPAIRED BS 328, LBL 37, WL 208 PER FED-EX EA NR 7-5310-36824.SDR 97FDEA00776Stringer · crackedNR 0417 007 AFT CARGO BAY AT BS 1113, STRINGER 28 R/H IS CRACKED ON INBOARD SIDE. *** S/D *** REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND PAINTED REPAIR PARTS. INSTALLED REPAIR PARTS FROM BS 1113 TO 1140, STR 20R. ALL IAW SDR 97FDEA00771Stringer · corrodedCORROSION (C53-113-01, 2) ON INBOARD SIDE OF STRINGER 28 RT, BS 1130. *S/D* REMOVED AND REPLACED STRINGER 28 RT IAW FED-EX SRM 53-10-3 FIG 1 SHT 1 WORK ACCOMPLISHED ON NR0417.SDR 97FDEA00768Spar Chord · corrodedCORROSION (C53-224-05) WING CENTER SECTION FRONT SPAR LOWER CHORD RBL 25, BS 740. *S/D* FOUND CORROSION OUT OF LIMITS. REMOVED WING CENTER SECTION FRONT SPAR LOWER CHORD. INSTALLED NEW CHORD IAW FED-EX EA- 7-5710-36858.SDR 97FDEA00761Wedge · delaminatedRT WING O/B MIDFLAP T/E WEDGE IS DELAMINATED 24 FROM I/B END AND AT THE NR 2 AFT FLAP TRACK, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.SDR 97FDEA00760Wedge · delaminatedLT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.SDR 97FDEA00755Bonding Jumper · corrodedNR 2 K-FLAP BULLNOSE CORRODED ON O/B BONDING JUMPER. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP O/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT IAW FED-EX SRM 57-50-3.SDR 97FDEA00742Wedge · delaminatedNR 0079 001, R/W I/B MIDFLAP T/E WEDGE IS DELAMINATED 16 FROM I/B END.SDR 97FDEA00664Clip · crackedNR 3 AND NR 4 LEFT HAND STRINGER CLIPS AT BS 1050 ARE CRACKED. *S/D* REMOVED CRACKED STRINGER CLIPS AT NR 3 AND NR 4 LT STRINGER AT BS 1050. INSTALLED NEW STRINGER CLIPS IAW FED-EX SRM 51-30-2, 51-10-1, M/M 25-52-2.SDR 97FDEA00656Skin · corrodedNR 0291 015 CORROSION ON UPPER SURFACE OF WING SKIN BS 850, LBL 82, WL 200. COMPLIED WITH EA 7-5730-35048.SDR 97FDEA00655Keel Beam · corrodedCORROSION (C53-113-01,1) ON RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148. *S/D* REPAIRED RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148 PER FED-EX EA 7-5310-35067.SDR 97FDEA00654Fire Loop · failedWW FIRE LIGHT CAME ON DURING APPROACH. LIGHT WENT OUT WHEN GEAR WAS LOWERED, TESTED OK. INSP RT AND LT WW FIRE LOOP, NO PHY DAMAGE FOUND. PERF WW FIRE TEST, ALL IND GOOD. DISCON AND MEG ALL 3 WW LOOPS. NOSE LOOP IS BD, READS .55 MEG SHD BE MORE THAN 5 MEGSDR 97FDEA00648Spoiler · delaminatedNR 0195 004 NR 2 SPOILER TRAILING EDGE IS DELAMINATED. REPAIRED NR 2 SPOILER IAW FED-EX SRM 57-50-06.SDR 97FDEA00647Skin · delaminatedLEFT WING I/B FOREFLAP HAS 6 X 6 AREA OF DELAMINATION ON UPPER I/B END. *S/D* REMOVED DAMAGED SKIN AND REPAIRED IAW FED SRM 51-40-6, LT I/B FOREFLAP.SDR 97FDEA00644Flap · delaminatedNR 0248 002 LEFT WING I/B MIDFLAP T/E WEDGE HAS AREA OF DELAMINATION ON O/B END. REMOVED DAMAGED AREA 9.25 BY 4 ON UPPER SURFACE OVERLAYED WITH RESIN IMPREGNATED FIBERGLASS, VACUUMED, BAGGED, SANDED, SEALED, PRIMED AND PAINTED L/T WING T/E WEDGE I/B MIDFLAP ISDR 97FDEA00643Flap · delaminatedNR 0249 001 RIGHT WING O/B MIDFLAP T/E WEDGE HAS TWO AREAS OF DELAMINATION ON UPPER SKIN. REMOVED DAMAGE 9 BY 3.5 OVERLAYED WITH RESIN IMPREGNATED FIBERGLASS VACUUM BAGGED. SANDED, SEALED, PRIMED AND PAINTED R/W O/B MIDFLAP IAW FED-EX SRM 51-40-06.SDR 97FDEA00639Clip · corrodedNR 0165 013 CORROSION (C53-224-05) ON T-CLIP, FWD SIDE, RBL 69, BS 760, WL 205. FOUND T CLIP TO BE CORRODED OUT OF LIMITS ON BS 760, WL 205, RBL 69. FABRICATED T CLIP AND INSTALLED IAW FED-EX SRM 53-30-5, 51-10-2, M/M 51-20-151, 51-20-21.SDR 97FDEA00638Frame · crackedCRACK ON UPPER FLANGE OF FRAME BS 1050, RBL 9, WL 155 ON PREVIOUS REPAIR, CRACK EXTENDS .5 BEYOND STOP DRILL HOLE. *S/D* CUT OUT DAMAGED FRAME SECTION AND REPAIRED PER FED-EX SRM 53-40-3.SDR 97FDEA00636Access Panel · corrodedNR 0167 012 CORROSION (C53-132-02(1)) ON 870 CENTER WING ACCESS PANEL, BS 870, LBL 4, WL 170. (INTERNAL TANK ACCESS IS REQUIRED.) REMOVED .020 CORROSION IN A 2.3 BY 11.9 AREA ORIGINAL THICKNESS .050 OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED SDR 97FDEA00630Hinge · corrodedCORROSION ON NR 1 K-FLAP CENTER HINGE LUG ON AIRCRAFT SIDE UNDER BOTH I/B AND O/B LUG SCREWS. REMOVED AND REPLACED NR 1 K-FLAP CENTER HINGE FITTING.SDR 97FDEA00610Flap · delaminatedLT WING I/B MIDFLAP T/E WEDGE DELAMINATED FROM 18 TO 26 FROM I/B END. *S/D* REPAIRED LT WING I/B MIDFLAP T/E WEDGE IAW FED-EX SRM 51-40-06 AND 51-30-02.SDR 97FDEA00609Stringer · corrodedCORROSION (C53-113-01,2) IN STR 27, RIGHT BS 970 TO 1035. *S/D* REMOVED CORROSION IN STR 27 RT, BS 970 TO 1035. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 27 RT, BS 970 TO 1035 PER FED-EX SRM 51-30-2, AND 51-10-1.SDR 97FDEA00607Stringer · corrodedCORROSION (C53-113-01, 2) IN STR 30, WL 148, BS 970 TO 1080. *S/D* REMOVED CORROSION IN STR 30, WL 148, BS 970 TO 1080. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 30, WL 148, BS 970 TO 1080 PER FED-EX SRM 53-10-3, 51-30-2, ASDR 97FDEA00606Spar Chord · corrodedCORROSION (C53-132-02- 1/2) WING CENTER SECTION LOWER FRONT SPAR CHORD BS 740, RBL 10 AND RBL 26 TO 30, WL 164.SDR 97FDEA00605Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, LBL 70 TO RBL 70, WL 188.SDR 97FDEA00604Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION LOWER REAR SPAR CHORD VERTICAL LEG BS 870, LBL 10 TO RBL 10, WL 164.SDR 97FDEA00603Angle · corrodedCORROSION (C53-224-05) ON RT 70.5 PREVIOUS REPAIR ANGLE, BS 754 TO 760, RBL 70.5, WL 204. *S/D* CORROSION ON ANGLE, BS 754 TO 760, OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED ANGLE PER FED-EX SRM 51-10-1.
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