Boeing 727-22

Service difficulty reports · 1,282

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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.

SDR 97FDEA00598Oil Filter · failedENGINE NR 2 SHUTDOWN IN FLIGHT, FILTER BYPASS LIGHT ILLUMINATED. PRESSURE ON GAUGE READ APPROXIMATELY 32 PSI, OIL QUANTITY NORMAL. REMOVED AND REPLACED NR 2 ENGINE MAIN OIL FILTER. FILTER BYPASS LIGHT REMAINED OUT, OIL PRESSURE NORMAL. LEAK CHECK GOOD.Aug 30, 1997 · N181FE · Boeing 72722 · Turbine Engine Oil SystemSDR 97FDEA00597Connectors · corrodedWHEEL WELL FIRE INDICATION ON DESCENT FL240, COMPLIED WITH RED TABS LIGHT WENT OUT. CRASH CREW CAME OUT AND INSPECTED ON LANDING, OK. REPEAT WRITE-UP. INSPECTED SENSING LOOPS IN NOSE AND MAIN WHEELS. CHECKED RESISTANCE PER CHAPTER 26-12-1 P 501 OF LOOPS, AAug 29, 1997 · N149FE · Boeing 72722 · Fire DetectionSDR 97FDEA00593Beam · corrodedNR 0308 003 CORROSION (C55-300-10-2) RT HORIZONTAL STAB UPPER T/E BEAM AT APPROX ELEV STA 147.5 (IN BALANCE BAY NR 4).Aug 28, 1997 · N166FE · Boeing 72722 · Horizontal Stabilizer StructureSDR 97FDEA00591Fire Loop · out of position97-0161 WHEEL WELL FIRE LIGHT ILLUMINATED ON FINAL TO MEM AT 150K/1200FT EXTINGUISHED MONENTARILY THEN REILLUMINATED COMPLIED WITH RED TABS. LIGHT AND BELL EXTINGUISHED JUST PRIOR TO LANDING GEAR BEING DROPPED. CIRCUIT TEST OK AFTER LANDING. NO EVIDENCE OF Aug 27, 1997 · N149FE · Boeing 72722 · Fire DetectionSDR 97FDEA00585Flap · delaminatedLEFT WING O/B MIDFLAP T/E WEDGE DELAMINATED IN SEVERAL AREAS FROM 17 TO 141 FROM I/B END. *S/D* REMOVED AND REPLACED LEFT WING OUTBOARD MIDFLAP IAW FED-EX M/M 27-51-11.Aug 26, 1997 · N166FE · Boeing 72722 · Trailing Edge FlapsSDR 97FDEA00584Flap · delaminatedRIGHT WING O/B MIDFLAP T/E WEDGE DELAMINATED FROM 66 TO 72 INCHES AND 115 TO 124 INCHES FROM O/B END. *S/D* REMOVED AND REPLACED RIGHT WING O/B MIDFLAP IAW FED M/M 27-51-13, DUE TO CORROSION ON MIDFLAP FRONT SPAR UPPER SURFACE.Aug 26, 1997 · N166FE · Boeing 72722 · Trailing Edge FlapsSDR CA970903001Engine · failed(CAN) DURING CLIMB THROUGH 10,000 FEET NOTICEABLE VIBRATION FELT FOLLOWED BY NR1 ENGINE OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATION. THRUST LEVER WAS RETARDED TO 60 PERCENT N1, LIGHT EXTINGUISHED. OIL PRESSURE AND TEMPERATURE WERE WITHIN LIMITS. 10 SECONDS LAug 22, 1997 · Boeing 72722 · Engine (Turbine/Turboprop)SDR 97FDEA00562Frame · crackedCRACK INDICATIONS NOTED (DAMAGED HOLE) BS 970, STR 27L AND 27R, AFT CARGO BAY LOWER LOBE. *S/D* REMOVED AREA OF DAMAGE .5 BY .5 BY .071 AT BS 970, STR 27L AND 27R, LOWER LOBE AND INSTALLED REPAIR DOUBLERS IAW FED-EX SRM 51-40-3.Aug 18, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00536Frame · crackedNR 0372 004 CRACK INDICATION NOTED AT TOOLING HOLE BS 1110, STR 26L AFT CARGO BAY LOWER LOBE. REMOVED .5 FT BY .3 FROM AREA AROUND TOOLING HOLE. REPAIRED IAW FED-EX SRM 51-40-3.Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00535Frame · damagedNR 0370 006 WHILE WORKING EO 7-5310-7-2354E2 PT 2, FOUND DAMAGED HOLES ON FRAME BS 1090, LBL 17, WL 150. REMOVED DAMAGED AREA OF .425 BY .550 AND .500 BY .750 ON FRAME BS 1090, LBL 17, WL 150. FABRICATED AND INSTALLED REPAIR PARTS PER FED-EX SRM 51-40-3.Aug 14, 1997 · N190FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00534Fitting · corrodedNR 0271 005 - R/W I/B AILERON, I/B TAB FITTING CORRODED (AREA MARKED).Aug 14, 1997 · N190FE · Boeing 72722 · AileronsSDR 97FDEA00521Shear Tie · corrodedCORROSION (C53-113-01, 2) BS 1168, AFT SHEAR TIE LBL 15 TO RBL 10 WL 164 BETWEEN STR 27R TO 27L. *S/D* REMOVED CORRODED SHEAR TIE AT BS 1168, LBL 15 TO RBL 10, WL 164. FABRICATED REPLACEMENT PART AND INSTALLED PER FED-EX SRM 51-10-1, 51-30-2.Aug 8, 1997 · N190FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00520Mid Flap · delaminatedRIGHT WING I/B MID FLAP T/E WEDGE IS DELAMINATED AT 22 INCHES FROM I/B END. *S/D* REMOVED 9 BY 4 OF DAMAGED SKIN AND CORE, 22 INCHES FROM I/B END OF RIGHT WING I/B MIDFLAP TRAILING EDGE WEDGE. FABRICATED AND INSTALLED REPAIR PER FED-EX SRM 51-40-6.Aug 8, 1997 · N190FE · Boeing 72722 · Trailing Edge FlapsSDR 97FDEA00504Skin · delaminatedNR 0011 001 R/W I/B FOREFLAP HAS DELAMINATION DENT APPROXIMATELY 48 I/B O/B END. REPAIRED R/W I/B FOREFLAP DELAMINATION DENT APX 48 I/B OF O/B END IAW FED-EX SRM 51-40-06.Aug 6, 1997 · N190FE · Boeing 72722 · Trailing Edge FlapsSDR 97FDEA00492Angle · crackedCORROSION (C53-224-05) AND CRACK ON LBL 70.5 PLUS CHORD REPAIR PARTS B STA 755 TO 760, WL 206 TO 203. *S/D* REMOVED DAMAGE AND REPAIRED LBL 70.5 PLUS CHORD REPAIR PARTS STA 755 TO 760, WL 206 TO 203 IAW FED-EX 7-5710-34961.Aug 1, 1997 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00484Angle · crackedNR 0239 008 ANGLE CRACKED AT FASTENER HOLE RT SIDE OF DRAG BRACE SHELF BS 336, RBL 20, WL 146.Jul 29, 1997 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR CA970811002Bolts · loose(CAN) ON POSITIONING FLIGHT AFTER C4 CHECK VIBRATION OF AIRFRAME WAS NOTED. FOUND ELEVATOR HINGE TO SPAR FITTING BOLTS LOOSE BUT DID NOT CONTRIBUTE TO VIBRATION.Jul 24, 1997 · Boeing 72722 · Elevator StructureSDR DHL97707003Accessory Unit · pin looseGOT GEAR WARNING HORN ON SHORT FINAL WHEN SELECTED TO FLAPS 30 AND THE HORN WOULD NOT SILENCE. FOUND PIN NR 7 ON LANDING GEAR ACCY UNIT, CONNECTOR D 1164 A MAKING INTERMITTENT CONTACT. REPLACED PIN, OPS CHECKED GOOD PER M/M 32-09-11.Jul 18, 1997 · N707DH · Boeing 72722 · Landing Gear Position and WarningSDR 97FDEA00457Stringer · corrodedNR 0385 007 CORROSION (C53-113-01(2)) ON STRINGER 29 LEFT AT BS 1084. REPAIRED CORROSION ON STRINGER 29L, BS 1084 IAW FED-EX SRM 53-10-3.Jul 17, 1997 · N185FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 97FDEA00445Keel Beam · corrodedSTR 29L KEEL BEAM AND SPLICE CORRODED BS 1030 TO 1090. *S/D* REMOVED DAMAGED KEEL BEAM 29L, BS 950 TO 1060. INSTALLED NEW KEEL BEAM AND REPAIRED DOUBLER ALL WORK DONE IAW FED-EX SRM 53-30-3, 53-10-4, 53-10-1, 51-10-1 M/M 32-12-1.Jul 17, 1997 · N185FE · Boeing 72722 · Fuselage Main, KeelSDR 97FDEA00435Frame · corrodedCORROSION (C53-224-05) ON BS 760 STUB BEAM, WEB LBL 65, WL 206. *S/D* REPAIRED STUD BEAM BS 760 LT SIDE, WL 206, LBL 65 PER FED-EX EA NR 7-5310-34968.Jul 14, 1997 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00425Clip · corrodedCORRODED STRINGER CLIP STR 25R, BS 380. *S/D* REMOVED CORROSION ON STR CLIP 25R, BS 380 IN AN AREA OF 1 X 2 X .010. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED STR CLIP IAW FED-EX SRM 51-10-2, 53-10-1.Jul 10, 1997 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00395Frame · crackedNR 0646 013 WHILE WORKING CUSTOMER CARD NR 0607, FOUND FRAME CRACKED BS 1110, WL 153, RBL 25. REPAIRED CRACKED FRAME AT BS 1110, WL 153, RBL 25. ALL WORK DONE PER FED-EX SRM 51-40-3.Jul 8, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00381Shear Tie · corrodedCORROSION ON SHEAR TIE BS 1130 BETWEEN STR 29L AND 30, AFT SIDE OF FRAME. *S/D* REMOVED CORRODED SHEAR TIE, FABRICATED SHEAR TIE AND ALODINED, PRIMED, AND INSTALLED SHEAR TIE AT BS 1130, STR 29L TO 30 IAW FED-EX SRM 53-10-4.Jun 30, 1997 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00380Spar Chord · corrodedCORROSION (C53132021/2, C53-224-050) ON LOWER 740 CENTER WING SPAR CHORD LBL-24 TO LBL 38 AND RBL 12 TO RBL 14. *S/D* REMOVED AND REPLACED LOWER BS 740 CENTER WING SPAR CHORD FROM LBL 70.5 TO RBL 70.5 AND REPAIRED CORRODED LOWER CENTER WING SKIN FROM LBL 25 Jun 30, 1997 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00432Chord · corrodedCORROSION ON 1176 REINFORCEMENT CHORD AT BS 1176, LBL 63, WL 208. *S/D* CUT OUT DAMAGED PORTION OF REINFORCEMENT CHORD AT BS 1176, LBL 32, 75 TO 63, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. LOCATED NEW CHORD SECTION, SPLICE PLATEJun 26, 1997 · N185FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00368Switch · dirty97-0114 AFTER TAKEOFF, MAIN CARGO DOOR LIGHT ILLUMINATED. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52 - 4A. VERIFY CARGO DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK OUT. CLEANED MAIN CARGO DOOR LOCK SWITCH. OPERATED DOOR NUMEROUS TIMES. OPERATION NORMAL. Jun 26, 1997 · N191FE · Boeing 72722 · Door Warning SystemSDR 97FDEA00365Frame · crackedCRACK IN FRAME BS 680, STR 22L IN FORWARD CARGO BAY. *S/D* REMOVED DAMAGED FRAME AREA 2.75 DIAMETER AREA. HFEC NOTED NO CRACKS FOUND. FABRICATED REPAIR PARTS FROM 7075-0 .050, IAW FED-EX SRM 51-40-3. TREATED AND PRIMED REPAIR PARTS PER FED-EX SRM 51-10-2.Jun 24, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00362Skin · disbondedSKIN IS DISBONDED AT BS 1143 TO 1166 BETWEEN STR 24R TO 25R. *S/D* ACCESSED AREA, REMOVED EXISTING DOUBLERS, REMOVED SKIN BS 1080 TO 1183, STR 20 TO 26R. DRILLED, TREATED MATERIAL AND INSTALLED. FABRICATED DOUBLERS, TREATED AND INSTALLED IAW FED-EA 7-5330Jun 20, 1997 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00361Chord · crackedRIGHT MAIN GEAR WELL, BS 950, RBL 3, WL 180, - 75 CRACK TOP OF AFT VERTICAL CHORD. *S/D* REMOVED DAMAGED VERTICAL CHORD, FABRICATED AND INSTALLED NEW VERTICAL CHORD AT BS 950, RBL 3, WL 150 TO 180 PER BOEING DRAWING 65-18636 AND FEDEX SRM 51-30-2.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00357Skin · disbondedNR 0577 007, SKIN IS DISBONDED AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20. *S/D* REPAIRED DISBONDED SKIN AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20 RT PER FED-EX SRM 53-30-4.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00356Stringer · corrodedNR 0124 008 CORROSION (C53-224-01(3)) ON STRINGER 2 RT AT BS 967. REPAIRED CORRODED STRINGER NR 2 RT AT BS 967. ALL WORK DONE PER FED-EX SRM 51-40 AND 53-10-3.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 97FDEA00350Floorbeam · corrodedNR 0573 006 WHILE WORKING NR 0172 FOUND CORROSION EMANATING FROM UNDER CEILING SUPPORT STRAP BS 540, RBL 25, WL 200. REPAIRED FLOORBEAM AT BS 540, RBL 25, WL 200 IAW FED-EX SRM 53-10-8.Jun 17, 1997 · N180FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 97FDEA00341Overheat Wire · looseLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FL 250 REFERRED TO RED TAB OK LIST PG 2-/-14. LIGHT EXTINGUISHED AFTER STEP 14. A CHECKLIST INDICATES LEAK BETWEEN BLEED VALVE AND PACK VALVE. FOUND SENSING ELEMENT DISCONNECTED FROM SUPPORT CLAMP AND DROPPING DOJun 14, 1997 · N181FE · Boeing 72722 · Overheat DetectionSDR 97FDEA00346Chord · corrodedNR 0571 004, CORROSION (C53-100-01,1) ON UPPER CHORD OF FRAME AT BS 220, RBL 21, WL 148. *S/D* REMOVED DAMAGED UPPER CHORD. FABRICATED AND INSTALLED NEW UPPER CHORD BS 220, RBL 28 TO LBL 28, WL 148 PER BOEING DRAWING 65-16305.Jun 13, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00338Floorbeam · corrodedNR 0215 002 CORROSION EMANATING FROM UNDER NUT PLATE BS 600 FLOORBEAM UPPER CHORD AT RBL 17, WL 208. REMOVED DAMAGED FLOORBEAM UPPER FLANGE REPAIRED PER FED-EX SRM 53-10-8 FIG 3.Jun 11, 1997 · N180FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 97FDEA00335Hyd Filter · dirtyON TAKEOFF, FIRST OFFICER FELT THAT HYDRAULIC PRESSURE TO ELEVATOR WAS LOST DURING GEAR RETRACTION. SAME THING OCCURED ON LANDING IN BFM WHEN SPEED BRAKES WERE DEPLOYED. DURING TAXI IN WAS ABLE TO DUPLICATE BY PULLING BACK ON YOKE WHILE SIMULTANEOUSLY DEPLOYJun 10, 1997 · N190FE · Boeing 72722 · Hydraulic Filter, MainSDR 97FDEA00347Frame · crackedNR 0558 005, FRAME CRACKED AT BS 680, STR 26R FWD CARGO BAY. *S/D* STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED AT BS 680, STR 26R AS PER FED-EX SRM 51-40-3.Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00345Angle · corrodedNR 0504 003, CORROSION ON SHEAR TIE AFT SIDE OF BS 660, STR 27 TO 28 RT. *S/D* REMOVED CORRODED SHEAR TIE ANGLE FROM BS 660 FRAME, AFT SIDE BETWEEN STR 27 TO 28 RT. CORROSION FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. FABRICATED, DRILLED, ALODINED, Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00329Frame · dentedNR 0502 001, BS 660 FRAME DENTED BETWEEN STR 24 TO 23 LT. *S/D* REPAIRED DENTED FRAME BS 660 BETWEEN STR 24 AND 23L PER FED-EX SRM 51-40-3.Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00360Beam · crackedNR 0214 FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN RADIUS ON AFT SIDE. REMOVED AND INSTALLED NEW FORWARD ENTRY DOOR LOWER GATE BEAM IAW FED-EX SRM 51-30-2, 51-30-5, AND 51-30-8.Jun 1, 1997 · N180FE · Boeing 72722 · Passenger/Crew DoorsSDR 97ZZZX2952Skin · corrosionDURING C-CHECK INSPECTION, DISCOVERED CORROSION COMMON TO THE LAP SEAM BETWEEN STA 259.5 AND STA 295 AND STR 24R. REPAIRED BY CLEANING OUT CORROSION PER SB 53-0072. DUE TO EXTENT OF DAMAGE, THE LAP SEAM WAS REPAIRED USING REPAIR DOUBLERS AND FILLERS. REPAIRMay 25, 1997 · N400RG · Boeing 72722 · Wing, Plate/SkinSDR 97FDEA00299Engine · failedPASSING 16,000 FEET ON DESCENT POWER AT IDLE, NR 2 ENGINE FLAMED OUT. ONLY ABNORMAL INDICATION WAS ZERO OIL PRESSURE. QUANTITY OK WITH N1 ROTATION. NO N2 WAS OBSERVED. FOUND OIL SCREEN FULL OF METAL. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 70T0502 AMay 21, 1997 · N169FE · Boeing 72722 · Engine (Turbine/Turboprop)SDR DHL97707002Hose · failedON DESCENT, S/O NOTED ILLUMINATION OF THE NR 1 B-HYDRAULIC ELECTRIC PUMP LIGHT. SHORTLY AFTERWARD, B-SYSTEM QTY BEGAN DROPPING AND WAS AT 0 BY LANDING. UPON LOWERING OF LANDING GEAR, A-SYSTEM QTY SLOWLY DROPPED. THEREAFTER, A-SYSTEM AND BRAKE PRESSURE REMAIMay 9, 1997 · N707DH · Boeing 72722 · Hydraulic System, MainSDR 97FDEA00253Shear Web · corrodedNR 0154 001 CORROSION (C53-224-08) ON SHEAR WEB AT BS 1162, RBL 48, WL 208. REMOVED CORROSION FROM SHEAR WEB AT BS 1162, RBL 48, WL 208. IN AN AREA OF 1.5 BY 1.5 BY .028, FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED DOUApr 29, 1997 · N192FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00242Gasket · leakingON CLIMBOUT, FIRE WARNING ON NR 3 ENGINE, REDUCED THROTTLE TO IDLE AND LIGHT WENT OUT. FOUND AIR LEAKING BAD AT 8TH STAGE CHECK VALVE AND 13TH STAGE DUCT. REMOVED AND REPLACED 8TH STAGE GASKET AND ENGINE TO PYLON 13TH STAGE DUCT. LEAK CHECKS GOOD, OK FOR SEApr 24, 1997 · N148FE · Boeing 72722 · Pneumatic Distribution SystemSDR 97FDEA00240Drive Motor · failedAT FLIGHT LEVEL 350 BOTH SYSTEM-A PRESSURE LIGHTS FLICKERED. SYSTEM-A PRESSURE WENT TO 0 EXECUTED LOSS HYDRAULIC CHECK LIST. SYSTEM-A FLUID SHUTOFFS WERE CLOSED AT 0410. REMOVED AND REPLACED OUTBOARD FLAP DRIVE MOTOR, OPERATIONAL CHECKS IN ACCORDANCE WITH Apr 24, 1997 · N194FE · Boeing 72722 · Trailing Edge Flap ActuatorSDR DHL97707001Dme Interrogator · inoperativeNR 2 DME IS INOP. MILEAGE DIFFERS FROM NR 1 DME FROM 20 MILES TO 150 MILES. FLAG COMES INTO VIEW INTERMITTENTLY. REMOVED AND REPLACED DME INTERROGATOR. OPS CHECK OK PER M/M.Apr 16, 1997 · N707DH · Boeing 72722 · DME/TACAN SystemSDR 97FDEA00178Panel · missingON TAKEOFF, A PYLON PANEL FELL OFF THE AIRCRAFT. MAINTENANCE RETRIEVED THE PANEL, NO OTHER ASSOCIATED PROBLEMS WITH AIRCRAFT. VERTICAL STABILIZER, FUSELAGE AND ENGINE COWLING INSPECTED, NO DAMAGE FOUND. MISSING PANEL INSTALLED ON UPPER SIDE OF NR 1 PYLON.Mar 17, 1997 · N105FE · Boeing 72722 · Nacelle/Pylon, Plate/SkinSDR 97FDEA00133Floorbeam · corrodedNR 0126 003 CORROSION (C53-224-03) ON FLOORBEAM LOWER CHORD AT BS 328, LBL 3, WL 200. REMOVED DAMAGE ON FLOORBEAM LOWER CHORD 1 INCH BY 1.5 INCH AT BS 328, LBL 3, WL 200. REPAIRED PER FED-EX SRM 53-10-8 FIG 7.Feb 28, 1997 · N148FE · Boeing 72722 · Fuselage Main, Floor Beam
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