N623FE

Service difficulty reports · 246

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 = 'N623FE' 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.

SDR FDEA201007152530Longeron Splice · crackedCTR CARGO BAY, BS 1537 L45R FOUND LONGERON SPLICE CRACKED. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINE FABRICATED AS PER DRAWING A5A7116 REV. D. THIS REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6-2-100 REV 110.Jul 15, 2010 · N623FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201007152529Longeron Splice · corrodedCTR. CARGO BAY, STA 1537 L44R FOUND LONGERON SPLICE CORROSION. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING A5A7114 REV J. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.Jul 15, 2010 · N623FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201007152528Longeron Splice · crackedCTR CARGO BAY BS 1537 LONGERON 44L FOUND LONGERON SPLICE CRACKED. CENTER CARGO COMPARTMENT STA 1537 44L LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING A5A 7116 REV. D. THIS REPAIR CLASSIFIED Jul 15, 2010 · N623FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201007152527Floor Support · crackedDURING WALK AROUND FOUND MAIN DECK FLOOR SUPPORT LOWER SURFACE AT STA 1887 X=25 FOUND CRACKED. MAIN DECK FLOOR SUPPORT AT STA 1887 X=25 REMOVED AND REPLACED AS PER SRM 51-31-01 REV 43. MACHINED NEW FLOOR SUPPORT AS PER DRAWING NR AGA 7081 REV. J. HOLES TRANSFJul 15, 2010 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201007152526Floor Support · corrodedDURING WALK AROUND FOUND MAIN DECK FLOOR SUPPORT LOWER SURFACE FROM STA 1887 TO 2007 X=-50 CORROSION AT SEVERAL LOCATIONS. MAIN DECK FLOOR SUPPORT AT STA 1887 TO 2007 X= -50 REMOVED AND REPLACED AS PER SRM 51-31-01 REV 43. MACHINE NEW FLOOR SUPPORT AS PER DRJul 15, 2010 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201007152525Seat Track · crackedMAIN DECK CARGO STA 5-83 X-=8 SEAT TRACK BASE FOUND CRACKED. CRACKED SEAT TRACK AT STA 5-83 X= 8 AREA REMOVED AS PER SRM 51-31-01 REV 43. NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-31-01 REV 43. PROTECTED AS PER SRM 51-21-01 REV 43. SEAT TRACK INSTALLED ASJul 15, 2010 · N623FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007122477Longeron Splice · crackedCTR CARGO COMPARTMENT STA 1537 LONGERON SPLICE FOUND CRACKED AT LONGERON 38L. REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 REV J. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.Jul 12, 2010 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201007122476Rib · crackedRT WING NR 16 L/E SLAT TRACK SUPPORT RIB FOUND SUSPECTED CRACK. CRACKED RIB NR 16 REMOVED AND REPLACED NEW RIB AT RH WING L/EDGE AS PER DOUGLAS DRAWING ARB7565 REV. C. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-10 REV 110. RH WING NR 8 SLAT CABLES ADJUSTMEJul 12, 2010 · N623FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200912304572Actuator · leakingDURING LEVEL FLIGHT, GOT LEVEL 1 ALERT "HYD 1 OFF", QUAN NR 1 2.7 & 520 PSI. TWO MINS LATER, HYD 1 QUAN LO, HYD 1R OFF & HYD PUMP 1L OFF AND "HYD 1 FAIL" ALERT. COMPLIED WITH QUH "HYD 1 OFF" AND "HYD 1 FAIL" CHECK LISTS. EXECUTED "NORMAL" LANDING AT HNL. Dec 30, 2009 · N623FE · Doug MD11F · Elevator Control SystemSDR 08FDEA04051Skin · chafedRIGHT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT DOUBLER INBOARD AND OUTBOARD LOWER SECTION FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER EA NR 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N623FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03864Rib · crackedLEFT WING, LEADING EDGE COMPARTMENT RIB AT XOS 1003 FOUND CRACK. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 13, 2008 · N623FE · Doug MD11F · Wing, Rib/BulkheadSDR 08FDEA03851Attach Bracket · crackedMAIN DECK CABIN, 1 OFF FRAME ATTACHMENT BRACKET AT APPROX FRAME STA 1259 LONGERON 15 FOUND CRACKED. NEW FRAME ATTACHMENT BRACKET FABRICATED AS PER EA 1-5740-122552, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 12, 2008 · N623FE · Doug MD11F · Fuselage Main, Attach FittingsSDR 08FDEA03850Door · chafedRIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT LOWER DOOR FWD SECTION FOUND CHAFED. REMOVED AND REPLACED WITH A FABRICATED DOOR AS PER AMM 27-80-30-4. DOOR FABRICATED AS PER EA 1-5740-122550, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 12, 2008 · N623FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR 08FDEA03806Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLSep 10, 2008 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03805Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLE D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR D AT NR 4 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-5Sep 10, 2008 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03804Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.Sep 10, 2008 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03803Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLE A. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR A AT NR 2 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-5Sep 10, 2008 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03802Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATION AT HOLES B, C AND D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLES B, C AND D AT NR 1 SUPPORT FITTING REPAIR CARRIED OUTSep 10, 2008 · N623FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03808Skin · chafedRIGHT WING LEADING EDGE LOWER SECTION AT STA XORS 372, INBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MARKS. CHAFE MARK SMOOTHED AND REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 10, 2008 · N623FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03807Skin · chafedRIGHT WING LEADING EDGE LOWER SECTION AT APPROX STA XORS 392, OUTBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 10, 2008 · N623FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03801Frame · crackedRT MAIN LANDING GEAR DOOR UPPER SIDE SURFACE CENTER FRAME CRACKED AT 2 LOCATIONS. REPAIRED AS PER EA 1-5280-123102, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 10, 2008 · N623FE · Doug MD11F · Landing Gear DoorsSDR 08FDEA03787Hinge · crackedRT MAIN LANDING GEAR DOOR FOUND CRACK ON CENTER HINGE. REMOVED AND REPLACED AS PER SRM 51-31-01.Sep 10, 2008 · N623FE · Doug MD11F · Landing Gear DoorsSDR 08FDEA03786Skin · chafedRIGHT WING NR 3 SLAT ASSY LOWER SECTION TRAILING EDGE FOUND WITH CHAFE MARKS. AREA REPAIRED AS PER EA 1-2780-122549, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 10, 2008 · N623FE · Doug MD11F · Leading Edge DevicesSDR 08FDEA03785Skin · dentedRT WING INBOARD FLAP LOWER SKIN CENTER AREA FOUND WITH SEVERAL DENTS. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 10, 2008 · N623FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA02654Pitot Tube · obstructedON TAKEOFF ROLL AIRSPEED INDICATORS DIFFERED BY 20 KNOTS REJECT T/O 04JUL08 09:12 TPE R. PERFORM PITOT TUBE PURGE ON AUX PITOT TUBE FOUND A BIG CLUNK OF MUD BLEW OUT THEN PERFORMED LEAK CHECK NORMAL PER MM 34-11-00-2.Jul 3, 2008 · N623FE · Doug MD11F · Pitot/Static SystemSDR 08FDEA00292Clamp · looseNR 2 ENG ANTI ICE DUCT LIGHT, SHUT DOWN NR 2 ENG AS DIRECTED BY CHECKLIST. REMOVED AND REPLACED ENG 2 ANTI-ICE VLV LATCHING (R2-5527) IAW MD-11 SMP. REMOVED AND REPLACED NR 2 ENG COWL ANTI-ICE MANIFOLD FAILURE SENSING ALL 3 LOOPS (D1-89, D1-90, AND D1-91) IAJan 26, 2008 · N623FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR 07FDEA01665Hinge Fitting · corrodedLT WING OUTBD FLAP INBD HINGE SUPPORT FITTING OUTBD AND 1 BOLT HOLE FOUND CORROSION. LT WING OUTBD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094 - WINGS, LT WING Apr 30, 2007 · N623FE · Doug MD11 · Leading Edge DevicesSDR 07FDEA01667Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01666Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01664Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 1 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01663Strut · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT (P/N: ARC2126) FWD AND AFT HOLE FOUND CORRODED. [SUP 05-15-07] COMPLIED WITH FEDEX E.A. 1-5750-111092.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01662Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORRODED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. COMPLY WITH FEDEX EA 1-5710-111094. REPAIR CApr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01661Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 2 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01619Skin · dentedFOUND LEFT WING, NR 3 SLAT LEADING EDGE FOUND DENT. [SUP 05-15-07] DENT ON NR 3 SLAT LEADING EDGE AT LEFT HAND WING SMOOTHENED OUT AND FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 16 VOLUME I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-111095, REPAIR IS CLApr 26, 2007 · N623FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA01546Stringer · crackedCRACK FOUND AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01545Stringer · crackedCRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01544Stringer · crackedCRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01543Stringer · crackedCRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. RApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01542Stringer · crackedCRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01541Stringer · crackedCRACK FOUND AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIApr 23, 2007 · N623FE · Doug MD11 · Wing, Longeron/StringerSDR 07FDEA01540Skin · crackedLEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-11-07] CRACK AT LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57- 10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 23, 2007 · N623FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA01539Skin · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-09-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 23, 2007 · N623FE · Doug MD11 · Wing, Plate/SkinSDR 05FDEA01749Skin · puncturedLT WING FIXED LE FOUND PUNCTURED AT XORS 402. PUNCTUREED SKIN ON LT WING FIXED L/E AT XORS402 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00, FIG 14, VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (OPEN)Jun 30, 2005 · N623FE · Doug MD11 · Wing, Plate/SkinSDR 05FDEA01743Panel · separatedLOST PANEL L WING COVERS OUTBD SLAT MECHANISM. LT WING PANEL NO.518FB REPLACED AS PER AMM 20-50-02 AND HINGE FILLERS REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.Jun 29, 2005 · N623FE · Doug MD11 · Leading Edge DevicesSDR 05FDEA01608Seat Track · crackedMAIN DECK, SEAT TRACK RBL 47 CRACKED AT STA 6-70. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 14, 2005 · N623FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01595Web · crackedRT OBSERVER SEAT CUT OUT FOUND CRACKED. CRACKED WEB AT COCKPIT FAC CARRIED OUT REPAIR AS PER SRM 53-00-01 VOLUME I, FIGURE 5 AT STA 366. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Jun 13, 2005 · N623FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01575Seat Track · crackedMAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 9, 2005 · N623FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01574Seat Track · crackedMAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 9, 2005 · N623FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01573Seat Track · crackedMAIN DECK, SEAT TRACK LBL 27 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 9, 2005 · N623FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01531Seat Track · crackedMAIN DECK, SEAT TRACK RBL 27 CRACKED AT STA 6-80. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 8, 2005 · N623FE · Doug MD11 · Fuselage Miscellaneous Structure
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