# Service difficulty reports: N315AA, cancelled Mar 8, 2016

A list on [N315AA, cancelled Mar 8, 2016](https://openairdocs.org/deregistered/N315AA-2016-03-08.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 112 reports

- [SDR ABXA20151014189](https://openairdocs.org/sdr/ABXA20151014189.md): Skin · corroded · Oct 14, 2015 · N315AA · Boeing 767223 · Fuselage Main, Plate/Skin
  > CORROSION ON LT FUSELAGE SKIN, STATION 955 C/T FAILSAFE TRIM OUT AREA GOING FWD UNDER FAILSAFE STRAP. FAIL SAFE REMOVED ON EA 53500013-008. REMOVED ALL CORROSION, NDT TESTED, NO DEFECTS NOTED. COMPLIED WITH EA 53500013-004 & REA B657-61768MR. REFERENCE EA
- [SDR ABXA20151013173](https://openairdocs.org/sdr/ABXA20151013173.md): Skin · corroded · Oct 13, 2015 · N315AA · Boeing 767223 · Fuselage Main, Plate/Skin
  > RIGHT STATION 18.09 PREVIOUS REPAIR DOUBLER, BETWEEN STRINGERS 9RT & 10RT. REQUEST ENGINEERING INSTRUCTIONS. REMOVED DOUBLER, CLEANED HOLES TO LEVEL 3, PERFORMED HFEC ON HOLES & AREA AROUND HOLES. PERFORMED GVI OF 22" AROUND 1809 REPAIR. FABRICATED RT DOUB
- [SDR ABXA20151012175](https://openairdocs.org/sdr/ABXA20151012175.md): Frame · cracked · Oct 12, 2015 · N315AA · Boeing 767223 · Fuselage Main, Frame
  > RIGHT FRAME INNER CHORD AT STATION 883.5, RBL 89 HAS A.250 CRACK IN TRANSITION RADIUS. REPAIRED CHORD IAW EA 53000050-101. CRACKED.50, PN 691T0003-44, PART NAME CHORD RT INNER, SN N/A, FS & BS LOCATION FROM 883.5 STRINGER & WS LOCATION RBL 89. ACFT WAS GN
- [SDR ABXA20151007190](https://openairdocs.org/sdr/ABXA20151007190.md): Tee Fitting · corroded · Oct 7, 2015 · N315AA · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > UPON CURSORY INSPECTION, FOUND CORROSION WITHIN AREA UNDER THIRD INBD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, APPROX NAC STATION 400. R & R CORRODED T FITTING IAW BCSF SRM 51-40-02 & DWG 313T1355. SDR INFO, CORRODED LEVEL 2, PN 313T1355-128, PART NAME T F
- [SDR ABXA20151003188](https://openairdocs.org/sdr/ABXA20151003188.md): Failsafe · cracked · Oct 3, 2015 · N315AA · Boeing 767223 · Fuselage Main, Frame
  > LEFT STATION 955, FAIL SAFE STRAP HAS.125 CRACK APPROX 2:00 POSITION AT THE BOTTOM FASTENER HOLE. LT FAIL SAFE STRAP IS BEING REPLACED. NEW FAIL SAFE STRAP PN 145T2524U21 TO BE INSTALLED ON EA53500013-008. SDR INFO CRACKED.125", PN 145T2524, PART NAME FAI
- [SDR ABXA20151002165](https://openairdocs.org/sdr/ABXA20151002165.md): Stiffener · corroded · Oct 2, 2015 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > LEFT WW AFT SPAR BULKHEAD FS 955, LBL 9, INBD VERTICAL ANGLE HAS TOOLING MARKS ON INBD SIDE IN NUMEROUS PLACES. BLENDED TOOLING MARKS ON REAR SPAR STIFFENER IAW REA 66740-MR. SDR INFO CORRODED, PN 111T 1005-1, SN N/A, PART NAME STIFFENER, LOCATION FROM STATI
- [SDR ABXA20151001170](https://openairdocs.org/sdr/ABXA20151001170.md): Longeron · corroded · Oct 1, 2015 · N315AA · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > CORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW, AROUND FASTENERS & ON FASTENER HEADS FROM FS 975 - 985. REMOVED CORROSION ORIGINAL.080, REMOVED.012, REMAINING.068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR
- [SDR ABXA20151001169](https://openairdocs.org/sdr/ABXA20151001169.md): Longeron · corroded · Oct 1, 2015 · N315AA · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > CORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW FROM FS 965 - 975. REMOVED CORROSION ORIGINAL.080, REMOVED.012, REMAINING.068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR INFO CORRODED LEVEL 2, PN 145T8800-20,
- [SDR ABXA20150930186](https://openairdocs.org/sdr/ABXA20150930186.md): Skin · corroded · Sep 30, 2015 · N315AA · Boeing 767223 · Wing, Plate/Skin
  > FOUND CORROSION AT APPROX WS 110 RT WING TE FLANGE. REMOVED CORROSION AT UPPER RT WING TE WBL110, PN 112T3101-6 IAW REA B657-61760-MR. SDR INFO, CORRODED LEVEL 2, PN 112T3101-6, SN NSN, PART NAME SKIN, FROM WS110. ACFT WAS GNDED.
- [SDR ABXA20150929168](https://openairdocs.org/sdr/ABXA20150929168.md): Longeron · corroded · Sep 29, 2015 · N315AA · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > LEFT WW FS APPROX 980 OVERWING LONGERON TOP SIDE HAS CORRODED FASTENERS & POSSIBLY AROUND BASE OF FASTENERS. REMOVED CORROSION, ORIGINAL MATERIAL.080, REMOVED.003, REMAINING.077 IAW REA B653-61756-MR, RFTS NR E-46344 REV DATE ER 9 23 15. SDR INFO CORRODED
- [SDR ABXA20150928187](https://openairdocs.org/sdr/ABXA20150928187.md): Failsafe · cracked · Sep 28, 2015 · N315AA · Boeing 767223 · Fuselage Main, Frame
  > FOUND CRACK AT LOWER OF 3 FASTENER HOLES INSPECTED. CRACK PLAINLY VISIBLE. REPAIRED AREA IAW DOCUMENT 470080RD06 & EA 53500014-003. SDR, CRACKED, LENGTH: 1.7 INCHES, PN 14T9524-22, PART NAME FAIL SAFE, SN NSN, FS & BS LOCATION SM 955, STRINGER & WS LOCATIO
- [SDR ABXA20150924191](https://openairdocs.org/sdr/ABXA20150924191.md): Angle · corroded · Sep 21, 2015 · N315AA · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > UPON CURSORY INSPECTION FOUND CORROSION WITHIN AREA UNDER FWD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, JUST ABOVE AFT EDGE OF EXHAUST NOZZLE, APPROX NAC STATION 350. R & R CORRODED ANGLE INSIDE OF FWD HEAT SHIELD PANEL AREA IAW SRM 51-40-02. SDR INFO, CORR
- [SDR ABXA20150918171](https://openairdocs.org/sdr/ABXA20150918171.md): Spar · corroded · Sep 18, 2015 · N315AA · Boeing 767223 · Wing Spar
  > CORROSION UNDER NUTPLATE ON UPPER CHORD OF WING REAR SPAR TO TE BEAM AT WING STATION 434, OTBD SIDE AS SEEN THRU PANEL 561AB. R & R UPPER CHORD OF WING REAR SPAR IAW SRM BCSF 51-40-02 PARA 7 D. SDR INFO CORRODED LEVEL 2, PN 113T1510-33, SN NSN, PART NAME CHO
- [SDR ABXA20150914185](https://openairdocs.org/sdr/ABXA20150914185.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 1, TENSION BOLT HOLE NR 1 HAS A DEFECT INDICATION, REFERENCE JC EA5750006-001. REAMED HOLE TO.672, NO FURTHER DEFECTS NOTED, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-43, PART NAME, FLAP SUPPORT FITTING NR 1,
- [SDR ABXA20150914184](https://openairdocs.org/sdr/ABXA20150914184.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 3 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED FASTENER HOLE TO.8285, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2,
- [SDR ABXA20150914183](https://openairdocs.org/sdr/ABXA20150914183.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED HOLE TO.829, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2, WS LOCATI
- [SDR ABXA20150914182](https://openairdocs.org/sdr/ABXA20150914182.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 1 HAS DEFECT INDICATION, REFERENCE JC EA57500018-001. REAMED FASTENER HOLE TO.8285, NO FURTHER DEFECTS, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR
- [SDR ABXA20150914181](https://openairdocs.org/sdr/ABXA20150914181.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 7, TENSION BOLT HOLE NR 4 HAS DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO.7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOC
- [SDR ABXA20150914180](https://openairdocs.org/sdr/ABXA20150914180.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > FLAP SUPPORT NR 7 TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO.7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOC
- [SDR ABXA20150914179](https://openairdocs.org/sdr/ABXA20150914179.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach Fittings
  > FLAP SUPPORT NR 7 TENSION BOLT HOLE 1 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO.7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING 7, WS LOCATIO
- [SDR ABXA20150914178](https://openairdocs.org/sdr/ABXA20150914178.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach Fittings
  > FLAP SUPPORT 8 TENSION BOLT HOLE 4 HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO.875, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCATION 798
- [SDR ABXA20150914177](https://openairdocs.org/sdr/ABXA20150914177.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach Fittings
  > NUMBER 8 FLAP SUPPORT TENSION BOLT HOLE 3 HAS A DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO.672, NO DEFECTS NOTED IAW REA B657-61078-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCA
- [SDR ABXA20150914176](https://openairdocs.org/sdr/ABXA20150914176.md): Support Fitting · corroded · Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach Fittings
  > NUMBER 8 FLAP SUPPORT TENSION BOLT HOLE NR 1, HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO.672, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-44, PART NAME, FLAP SUPPORT FITTING NR 8, WS
- [SDR ABXA20150910172](https://openairdocs.org/sdr/ABXA20150910172.md): Beam · cracked · Sep 10, 2015 · N315AA · Boeing 767223 · Nacelle/Pylon, Main Frame
  > NUMBER 2 STRUT INSIDE PANEL 447BR, LOWER BEAM IS CHAFED & CRACKED AT THIRD HOLE FROM THE FWD END. R & R LOWER BEAM INSIDE NR 2 PYLON PANEL 447BR IAW SRM 54-51-71 & DWG 313T2380. SDR INFO, PN 313T2380-29, PART NAME, BEAM, SN NSN, CRACKED.5 INCHES, EXACT FS &
- [SDR ABXA20140915293](https://openairdocs.org/sdr/ABXA20140915293.md): Inverter · damaged · Sep 15, 2014 · N315AA · Boeing 767223 · DC Rectifier/Converter
  > CREW REPORTED EICAS MESSAGE STBY INVERTER DISPLAYED, SMOKE IN THE CABIN & A STRONG ELEC BURNING ODOR. THE FLIGHT WAS DIVERTED TO NEAREST SUITABLE AIRPORT. THE STATIC INVERTER WAS REPLACED IAW AMM. 767 FAULT ISOLATION MANUAL PROCEDURES 24-33-807 808 WERE ACC
- [SDR ABXA20140910291](https://openairdocs.org/sdr/ABXA20140910291.md): Engine · bird ingestion · Sep 10, 2014 · N315AA · Boeing 767223 · Turbine Engine Compressor Section
  > ON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. RE
- [SDR ABXA20131213659](https://openairdocs.org/sdr/ABXA20131213659.md): Power Supply · shorted · Dec 11, 2013 · N315AA · Boeing 767223 · Flight Management Computing Hardware System
  > DURING EXTENDED GROUND TAXI, LT FLIGHT MANAGEMENT COMPUTER FAILED MESSAGE DISPLAYED, FOLLOWED BY SMOKE FROM THE LT CDU & THE LT CDU CIRCUIT BREAKER TRIPPED OPEN. THE CDU WAS REMOVED FOR INSPECTION & NO DAMAGE TO THE WIRING OR CONNECTORS ASSOCIATED WITH THE CD
- [SDR ABXA20131106643](https://openairdocs.org/sdr/ABXA20131106643.md): Rib · cracked · Nov 6, 2013 · N315AA · Boeing 767223 · Wing, Rib/Bulkhead
  > LEFT WING MAIN TRACK RIB AT OSS 1094 IS CRACKED WHERE TRACK BEARING ATTACHES. REMOVED DAMAGE IAW BCSF 767-200 57-41-09 FIG 101 & COMPLIED WITH RGA NR B657 - 60775 MR. CRACKED 1/2 INCH, LOC AT OSS 1094, PN 114T2118-7, PN RIB, SN NA. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131106634](https://openairdocs.org/sdr/ABXA20131106634.md): Fairing · cracked · Nov 6, 2013 · N315AA · Boeing 767223 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER AFT AT BASE UNDER 324AL METAL CHAFED & KNIFE EDGED. SRM 51-40-02 APPLIED TOP COAT IAW BOE 767 SRM 51-20-00. CRACKED CHAFED 4 INCHES, LOC FROM 1746 TO 1767, PN 148T7501017, PN FAIRING, SN NA. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131105644](https://openairdocs.org/sdr/ABXA20131105644.md): Rib · cracked · Nov 5, 2013 · N315AA · Boeing 767223 · Wing, Rib/Bulkhead
  > LEFT WING MAIN TRACK RIB AT OSS 1097 IS CRACKED WHERE THE TRACK BEARING ATTACHES. R & R IAW B767-200 SR SRM 51-40-02, REPAIRED 21E1 IAW REA NR B657-60774 MR. PN 114T2119-1 SN NSN CRACKED LENGTH.125, PN ASSEMBLY RIB STR & WS LOCATION AT OSS 1097. AIRCRAFT W
- [SDR ABXA20131105635](https://openairdocs.org/sdr/ABXA20131105635.md): Stringer Clip · cracked · Nov 5, 2013 · N315AA · Boeing 767223 · Fuselage Main, Attach Fittings
  > CLIP ON STRINGER 2 RT AT STATION 1678 CRACKED. R & R CLIP IAW DRAWING 148T1121 & SRM 51-20- 02. PN 148T1303-1 SN NA CRACKED 1/4 INCH, PN CLIP FS & BS LOCATION 1678 TO 1678 STRINGER & WS LOCATION R2 TO R2. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131104641](https://openairdocs.org/sdr/ABXA20131104641.md): Intercostal · corroded · Nov 4, 2013 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 549 RBL 6 THE STRUCTURE FOR THE LATERAL GUIDE NUTPLATES IS CORRODED. R & R 452T2704-1 INTERCOSTAL IAW DRAWING 451T2501 & SRM 51-40-02. R & R WEB FLOOR FS 522 - 549 RBL12 - LBL12 & INSTALLED LATERAL GUIDE AT FS 549 RBL 6 IA
- [SDR ABXA20131104627](https://openairdocs.org/sdr/ABXA20131104627.md): Structure · corroded · Nov 4, 2013 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 412 LBL 46 LOWER SIDE OF UPPER CHORD, BELOW CARGO FLOOR, IS SPLIT WITH INTERNAL CORROSION AT NUTPLATE LOCATION. REMOVED PDU L1 & L2, REMOVED ROLLER TRAYS. R & R DRILLED & INSTALLED CORD PT STATION 412, REINSTALLED ROLLER
- [SDR ABXA20131102642](https://openairdocs.org/sdr/ABXA20131102642.md): Plate · cracked · Nov 2, 2013 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > UPPER CARGO FLOOR PANEL MOUNTING PLATE UNDER CARGO LOCK MOUNT IS CRACKED FS 1021 LBL 45. R & R MATCH DRILLED TO FLOOR PANEL, FLOOR PANEL MOUNTING PATE AT FS 1021 LBC 45 IAW B767 SRM 51-40-02, 51-40-05, PN PLATE, CRACK LENGTH 1 INCH, PN 457T4101-2, SN NSN, LOC
- [SDR ABXA20131101632](https://openairdocs.org/sdr/ABXA20131101632.md): Keelbeam · corroded · Nov 1, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON FLAT PANEL IN WW AT STATION 973 LBL 6 & ON ANGLE AT STATION 977 LBL 6. REMOVED CORROSION IAW B767-200 SRM 53-50-12. COMPLIED WITH REA NR B653-60754-MR. PN 145T8612-1, PN KEEL BEAM WEB FS & BS LOC. ON A/C BS 973 TO BS 977, STRINGER & WS LOC. ON
- [SDR ABXA20131101629](https://openairdocs.org/sdr/ABXA20131101629.md): Frame · corroded · Nov 1, 2013 · N315AA · Boeing 767223 · Fuselage Main, Frame
  > FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 20 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. REMOVED OLD CORD DRILLED NEW ONE IAW BOE 767 SRM 51-40-05 INSTALLED NEW CORD IAW BOE 767 SRM 51-40-02, OLD CORD WAS FOUND TO BE OUT OF LIMITS IAW
- [SDR ABXA20131101628](https://openairdocs.org/sdr/ABXA20131101628.md): Frame · corroded · Nov 1, 2013 · N315AA · Boeing 767223 · Fuselage Main, Frame
  > FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 38 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. R & R CORD ON NR 0259. NEW CORD WAS DRILLED IAW BOE 767 SRM 51-40-05 ROLLER TRAYS WILL BE REINSTALLED ON NR 0250 ENTRY 4 CORD WAS OUT OF LIMITS I
- [SDR ABXA20131031638](https://openairdocs.org/sdr/ABXA20131031638.md): Shear Tie · corroded · Oct 31, 2013 · N315AA · Boeing 767223 · Fuselage Internal Mounting Structure
  > AREA BEHIND FWD LOWER CARGO AT FUSELAGE STATION 742 STRINGER 38L - STRINGER 39L SHEAR TIE CORRODED. INSTALLED SHEER TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN 538L & 539L IAW B767 SRM 51-40-02. LEVEL 2 CORRODED, LOC FROM 742, LOC FROM 538L TO 539L, PN 140
- [SDR ABXA20131031636](https://openairdocs.org/sdr/ABXA20131031636.md): Shear Tie · corroded · Oct 31, 2013 · N315AA · Boeing 767223 · Fuselage Internal Mounting Structure
  > BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 35L - STRINGER 36L. INSTALLED NEW SHEET TIE IN FWD LOWER CARGO AT STATION 742 BETWEEN STRINGER 35L - STRINGER 36L IAW B767 SRM 51- 40-02. LEVEL 2, LOC FROM 742, LOC.
- [SDR ABXA20131030631](https://openairdocs.org/sdr/ABXA20131030631.md): Floorbeam · corroded · Oct 30, 2013 · N315AA · Boeing 767223 · Fuselage Main, Floor Beam
  > FORWARD LOWER CARGO FUSELAGE STATION 720 LBL 41 UPPER & LOWER CHORD IS CORRODED & SEPARATING INCLUDING 3 INCHES OTBD ON LOWER SIDE. REPLACED T CHORD. LOCATED, DRILLED & INSTALLED IAW DRAWING 143T1213. LEVEL 2 CORROSION LOC FROM FS 720 LBL43 TO FS 720 RBL 43,
- [SDR ABXA20131030630](https://openairdocs.org/sdr/ABXA20131030630.md): Intercostal · corroded · Oct 30, 2013 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 580 LBL 13 ON LOWER SIDE OF INTERCOSTAL CORRODED. REPLACED & INSTALLED NEW INTERCOSTAL AT STATION S80 LBL 13 IAW B767 SRM 51-40- 02 & IAW B767 SRM 53-00-04, INSTALLED PDO AT STATION 580 LBL 13 IAW B767 AMM 25-53- 0. LEVEL
- [SDR ABXA20131029640](https://openairdocs.org/sdr/ABXA20131029640.md): Panel · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 630 BILGE PANEL COVER CORRODED ON TOP AT LBL PO 0039309. LEVEL 2 CORROSION PN 143T5000-122, PN BILGE PANEL, SN NA. LOCATION FROM 632 TO 610 LOCATION FROM LBL 11 TO LNL 11. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131029637](https://openairdocs.org/sdr/ABXA20131029637.md): Shear Tie · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Internal Mounting Structure
  > BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 38R - STRINGER 39R. R & R SHEAR TIE AT STATION 742 BETWEEN G38R & 39R IAW B767-200 SRM 51-40-02. LEVEL 2 CORROSION, PN 140T2102U254, PN SHEAR TIE, SN NSN, LOC FROM 74
- [SDR ABXA20131029633](https://openairdocs.org/sdr/ABXA20131029633.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > LEFT HAND KEEL CHORD UPPER FLANGE HAS CORROSION AT STATION 985 - 995 LBL 10.75. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 985 -FS 995, LBL 10.75 TO L
- [SDR ABXA20131029626](https://openairdocs.org/sdr/ABXA20131029626.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM UPPER & LOWER SURFACE ADJACENT TO NUTPLATE AT STATION 801 LBL 9. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC FS 801, LBL 9. AIRCRAFT
- [SDR ABXA20131029625](https://openairdocs.org/sdr/ABXA20131029625.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > SPOT OF CORROSION ON KEEL BEAM UPPER SURFACE AT STATION 814 RBL 9 ADJACENT TO NUTPLATE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101. COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC 814 RBL 9. AIRCRAFT WA
- [SDR ABXA20131029624](https://openairdocs.org/sdr/ABXA20131029624.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM AT STATION 827 LBL 11. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD LT, SN NA, LOC FS 827, LBL 11. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131029623](https://openairdocs.org/sdr/ABXA20131029623.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM AT STATION 955 LBL 12. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5, PN KEEL BEAM CHORD, SN NA, LOC FS 955, LBL 12. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131029622](https://openairdocs.org/sdr/ABXA20131029622.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM AT STATION 951 RBL 12 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-65, PN KEEL BEAM CHORD, SN NA, LOC FS 951 RBL 12, AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131029621](https://openairdocs.org/sdr/ABXA20131029621.md): Keelbeam · corroded · Oct 29, 2013 · N315AA · Boeing 767223 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM AT STATION 808 RBL 10 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-6, PN KEEL BEAM CHORD, SN NA, LOC STATION 808 RBL 10, AIRCRAFT WAS GROUNDED.

Next page: https://openairdocs.org/deregistered/N315AA-2016-03-08/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N315AA' AND deregistration_id = 'N315AA-2016-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N315AA-2016-03-08/reports

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